GeeSat — 2024-023
launch attemptOrbital attemptcompleted
GeeSat — 2024-023 was an orbital attempt conducted on February 2, 2024 from XSC using Chang Zheng 2C, operated by Chinese Academy of Launch Vehicle Technology (CASC 1st Acad) and carrying 11 recorded payload entries. The recorded outcome was success; the census identity distinguishes this attempt from flights that may share a mission name or launch date.
- Launch class
- Orbital attempt
- Launch date
- February 2, 2024
14 related records 1 source
The Long March 2F carrying Shenzhou 13 rises beside the launch tower at night
Credit: ForrestXYC; post-processing by Ib. License: CC BY-SA 4.0; credit ForrestXYC and Ib. Source-disclosed post-processing is retained without further content alteration in responsive copies..
Image source and licenseAbout this image
The Wikimedia Commons file record identifies this photograph as the Shenzhou 13 launch at Jiuquan on October 16, 2021 local time (October 15 UTC, matching the archive event); the frame visibly shows the mission's Long March 2F rising under power. The source explicitly discloses post-processing by Ib.
About this launch
All launches targeting a positive-perigee Earth orbit, including success, partial success, failure, and pre-liftoff pad explosion. This launch is retained as its own historical attempt so its date, vehicle, origin, operator, trajectory, payload, and outcome can be followed without collapsing it into a program total.
GeeSat — 2024-023 used Chang Zheng 2C from XSC under Chinese Academy of Launch Vehicle Technology (CASC 1st Acad). The technical record includes a recorded apogee of 606 km, a recorded perigee of 592 km, an inclination of 0°, the Sat LEO O profile. 11 payload entries are connected to the launch manifest.
Launch facts
- Launch date
- February 2, 2024
- Vehicle
- Chang Zheng 2C
- Outcome
- success
- Launch site
- XSC
- Operator
- Chinese Academy of Launch Vehicle Technology (CASC 1st Acad)
Technical details and catalog designation
Trajectory measurements and catalog terminology are retained here when available. Codes follow the original records.
- Launch class
- Orbital attempt
- Destination / profile
- Sat LEO O
- Recorded apogee
- 606 km
- Recorded perigee
- 592 km
- Inclination
- 0°
- Payload entries
- 11
- Catalog designation
- 2024-023
Payload manifest
GeeSAT 2-01
2024-023A · S58905 · GEESP
GeeSAT 2-02
2024-023B · S58906 · GEESP
GeeSAT 2-03
2024-023C · S58907 · GEESP
GeeSAT 2-04
2024-023D · S58908 · GEESP
GeeSAT 2-05
2024-023E · S58909 · GEESP
GeeSAT 2-06
2024-023F · S58910 · GEESP
GeeSAT 2-07
2024-023G · S58911 · GEESP
GeeSAT 2-08
2024-023H · S58912 · GEESP
GeeSAT 2-09
2024-023J · S58913 · GEESP
GeeSAT 2-10
2024-023K · S58914 · GEESP
GeeSAT 2-11
2024-023L · S58915 · GEESP
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From GeeSat — 2024-023
Spacecraft and hardware
- GeeSAT 2-01Payload manifest entry
- GeeSAT 2-02Payload manifest entry
- GeeSAT 2-03Payload manifest entry
- GeeSAT 2-04Payload manifest entry
- GeeSAT 2-05Payload manifest entry
- GeeSAT 2-06Payload manifest entry
- GeeSAT 2-07Payload manifest entry
- GeeSAT 2-08Payload manifest entry
- GeeSAT 2-09Payload manifest entry
- GeeSAT 2-10Payload manifest entry
- GeeSAT 2-11Payload manifest entry
Places and facilities
Other names mentioned
- Chang Zheng 2CLaunch vehicle
Listed without a linked page
- Chinese Academy of Launch Vehicle Technology (CASC 1st Acad)Launch operator
Listed without a linked page
Sources
Original references supporting this record. Each source opens on its publisher’s website.