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: 1 day ago
TLE from 1 day ago
0 GITAI-SC1
1 62388U 24247M 26093.11170873 .00011532 00000-0 52841-3 0 9999
2 62388 45.0030 357.3541 0000552 279.1445 80.9372 15.20600349 71303Epoch: 2026-04-03T02:40Z
TLE epoch observation values (Epoch: 2026-04-03T02:40:51.634Z)
Latitude
-0.00008°
Longitude
125.68836°
Altitude
503.968 km
Speed
7.614 km/s
True Right ascension
23h 49m 24s
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
19:10:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.012 km
Perigee altitude
505.252 km
Semi-major axis
6,883.769 km
Eccentricity
0.00006
Inclination
45.003°
RAAN
357.3541°
Arg. of periapsis
279.1445°
True anomaly
80.94345°
Mean anomaly
80.9372°
Eccentric anomaly
80.94032°
Mean motion
3.80018 °/min
Orbital period
94.73 mins
BSTAR
0.00052841
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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 | 2026-04-04 19:51:53.203Z | 198.21° SSW | 2026-04-04 19:53:53.203Z | 159.015° S | 25.925° | 2026-04-04 19:56:53.203Z | 90.084° ESE |
| 6 mins | 2026-04-04 21:30:53.203Z | 262.098° W | 2026-04-04 21:33:53.203Z | 20.385° NNE | 40.505° | 2026-04-04 21:36:53.203Z | 62.703° ENE |
| 5 mins | 2026-04-04 23:10:53.203Z | 301.705° NW | 2026-04-04 23:12:53.203Z | 351.434° N | 31.206° | 2026-04-04 23:15:53.203Z | 63.168° ENE |
| 5 mins | 2026-04-05 00:50:53.203Z | 306.837° NW | 2026-04-05 00:52:53.203Z | 30.426° NE | 40.822° | 2026-04-05 00:55:53.203Z | 96.937° ESE |
| 5 mins | 2026-04-05 02:29:53.203Z | 265.572° W | 2026-04-05 02:31:53.203Z | 214.236° SW | 29.008° | 2026-04-05 02:34:53.203Z | 152.64° 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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