Lesson 1 of 4 · Choose a view of the sky
Choose a view of the sky
6 minute lesson · 3 checks along the way
Your goal for this lessonExplain how NEOSSat’s geometry and shared mission determine which observations are possible.
In this lesson 3 sections · 3 checks
Using archive links & definitions
Follow a linked name to explore its archive card. “Back to your lesson” brings you to the same part of the reading.
Read & understand
One telescope, two research roles
NEOSSat, the Near-Earth Object Surveillance Satellite, launched on February 25, 2013. Its small telescope serves a Canadian partnership: the Canadian Space Agency leads astronomy work, while Defence Research and Development Canada leads the High Earth Orbit Space Surveillance research mission, or HEOSS. Sharing a spacecraft does not make those observing programs interchangeable.
The astronomy work includes measurements of asteroids, comets and stars with transiting planets. HEOSS investigates human-made objects in Earth orbit. The historical astronomy guest call used here excludes proposals to image satellites, debris or Earth. That is a boundary of the particular guest program, not proof that the spacecraft lacks other capabilities.
The NEOSSat archive card connects this course to the actual spacecraft. Its integration photograph shows the long telescope baffle projecting from the body. The baffle limits unwanted light entering the instrument; it does not enlarge the collecting aperture. A small aperture still needs adequate exposure, pointing and detector calibration to produce useful measurements.
NEOSSat during integration testing, from Figure 2 of the mission-team report The NEOSSat Experience. The extended baffle helps control unwanted light. This is a ground-test photograph, not an orbital view. Full embedded image retained at its publication resolution.
Look closely
What does the extended structure in front of the telescope help control?
See what to notice
The baffle restricts unwanted incoming light; its length does not make the telescope’s collecting aperture larger.
Check 1 of 3
10 pointsUse the reading above. You can try again without losing points.
Read & understand
Near the Sun means an angle on the sky
Solar elongation is the apparent angle between a target and the Sun as seen by the observer. It is not the target’s physical distance from the Sun. Objects at very different distances can appear in nearly the same direction. A useful observation plan therefore separates sky geometry from the orbit one hopes to infer.
NEOSSat can observe some low-elongation targets that are difficult from the ground. Its orbital location avoids terrestrial weather, but Earth, bright sources, thermal conditions and spacecraft operations still constrain the view. A claim that an observatory can work around the clock does not mean that every selected target is continuously visible.
For an original planning exercise, suppose a fictional instrument rejects directions closer than 40 degrees to the Sun under a stated mode. Targets at 25 and 55 degrees fall on different sides of that one limit. The 55-degree target passes this test, but passing one test does not establish that all other requirements are met. These numbers are a simplified exercise, not instructions for commanding NEOSSat.
Find the usable exposure time
Original teaching diagram. Invented schedule; not a NEOSSat command plan.
Open full-size diagram in a new tab: Find the usable exposure timeCheck 2 of 3
10 pointsUse the reading above. You can try again without losing points.
Read & understand
Count usable time, not simply orbital time
A target may disappear behind Earth, enter a region of higher particle background or require a pointing transition. Some interruptions remove data entirely; others leave exposures whose quality must be checked. An observation log should distinguish missing measurements from rejected measurements and usable ones.
In a fictional 100-minute planning interval, a target is geometrically accessible for 65 minutes. Repointing and settling consume another 5 of those minutes, leaving at most 60 for the intended exposure sequence. The usable fraction is 60 percent of the interval before any later quality rejection. Adding unavailable minutes to exposure time would give a misleading sensitivity estimate.
The practical question is whether the remaining samples can answer the science question. A short asteroid position measurement and an uninterrupted record of a transit may need very different schedules. Start with the required measurement, then examine visibility and operations together.
Check 3 of 3
10 pointsUse the reading above. You can try again without losing points.
Put it together
Your lesson progress
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Explore further · Optional
Go to the source
Explore the evidence behind this lesson. These optional readings and videos open in a new tab.
- Read: CSA: NEOSSat mission and astronomy research
- Read: CSA: historical guest observation cycle 10 requirementsHistorical cycle: December 1, 2025–March 31, 2026. Instrument constraints describe that call; this is not a currently open application.
- Read: NEOSSat mission team: five-year engineering and observing experienceHistorical mission-team account; recovery events and observing examples are dated evidence, not a live status feed.