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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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: 13 hours ago
TLE from 13 hours ago
0 GITAI-SC1
1 62388U 24247M 26221.81796573 .00002411 00000-0 11622-3 0 9998
2 62388 45.0024 21.5366 0001975 269.8132 90.2523 15.21850687 90902Epoch: 2026-08-09T19:37Z
TLE epoch observation values (Epoch: 2026-08-09T19:37:52.239Z)
Latitude
0.00003°
Longitude
128.75946°
Altitude
500.264 km
Speed
7.616 km/s
True Right ascension
01h 26m 08s
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
22:54:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.222 km
Perigee altitude
500.505 km
Semi-major axis
6,880 km
Eccentricity
0.0002
Inclination
45.0024°
RAAN
21.5366°
Arg. of periapsis
269.8132°
True anomaly
90.27493°
Mean anomaly
90.2523°
Eccentric anomaly
90.26362°
Mean motion
3.8033 °/min
Orbital period
94.65 mins
BSTAR
0.00011622
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-08-10 13:08:12.393Z | 189.623° SSW | 2026-08-10 13:11:12.393Z | 131.912° SE | 20.508° | 2026-08-10 13:13:12.393Z | 96.09° ESE |
| 6 mins | 2026-08-10 14:47:12.393Z | 252.05° W | 2026-08-10 14:49:12.393Z | 271.607° WNW | 42.362° | 2026-08-10 14:53:12.393Z | 64.938° ENE |
| 5 mins | 2026-08-10 16:27:12.393Z | 300.69° NW | 2026-08-10 16:29:12.393Z | 357.758° N | 31.769° | 2026-08-10 16:32:12.393Z | 62.277° ENE |
| 6 mins | 2026-08-10 18:06:12.393Z | 303.508° NW | 2026-08-10 18:09:12.393Z | 39.7° NE | 36.655° | 2026-08-10 18:12:12.393Z | 90.578° ESE |
| 5 mins | 2026-08-10 19:46:12.393Z | 269.457° W | 2026-08-10 19:48:12.393Z | 199.01° SSW | 34.995° | 2026-08-10 19:51:12.393Z | 140.565° 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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