GITAI-SC1, 62388
Orbit data source: Space-Track
GITAI-SC1, 62388 is a payload satellite owned by GITAI USA (US) in LEO that was launched on Sat, 21 Dec 2024 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62388 intel report (Beta)
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GITAI-SC1 radio frequencies
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GITAI USA
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 GITAI-SC1
1 62388U 24247M 25264.21858052 .00006739 00000-0 32399-3 0 9990
2 62388 45.0017 323.3649 0002341 315.5423 44.5268 15.19525647 41806Epoch: 2025-09-21T05:14Z
TLE epoch observation values (Epoch: 2025-09-21T05:14:45.356Z)
Latitude
-0.0001°
Longitude
-115.66445°
Altitude
506.123 km
Speed
7.613 km/s
True Right ascension
21h 33m 27s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:10:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
510.489 km
Perigee altitude
507.264 km
Semi-major axis
6,887.013 km
Eccentricity
0.00023
Inclination
45.0017°
RAAN
323.3649°
Arg. of periapsis
315.5423°
True anomaly
44.54562°
Mean anomaly
44.5268°
Eccentric anomaly
44.53621°
Mean motion
3.79749 °/min
Orbital period
94.8 mins
BSTAR
0.00032399
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Other satellites on launch #247 in the year 2024 (2024-12-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.GITAI-SC1 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-22 06:40:22.538Z | 206.547° SW | 2025-09-22 06:43:22.538Z | 149.604° SSE | 27.942° | 2025-09-22 06:46:22.538Z | 85.783° E |
| 6 mins | 2025-09-22 08:20:22.538Z | 265.477° W | 2025-09-22 08:22:22.538Z | 312.913° NW | 40.681° | 2025-09-22 08:26:22.538Z | 63.032° ENE |
| 5 mins | 2025-09-22 10:00:22.538Z | 304.327° NW | 2025-09-22 10:02:22.538Z | 357.926° N | 31.476° | 2025-09-22 10:05:22.538Z | 65.07° ENE |
| 6 mins | 2025-09-22 11:39:22.538Z | 299.953° NW | 2025-09-22 11:42:22.538Z | 39.442° NE | 41.317° | 2025-09-22 11:45:22.538Z | 99.05° ESE |
| 5 mins | 2025-09-22 13:19:22.538Z | 263.728° W | 2025-09-22 13:21:22.538Z | 213.905° SW | 27.731° | 2025-09-22 13:24:22.538Z | 154.776° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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