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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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: 13 hours ago
TLE from 13 hours ago
0 GITAI-SC1
1 62388U 24247M 26036.73109696 .00009990 00000-0 46924-3 0 9999
2 62388 45.0029 301.6738 0000106 77.3968 282.6924 15.19876816 62726Epoch: 2026-02-05T17:32Z
TLE epoch observation values (Epoch: 2026-02-05T17:32:46.777Z)
Latitude
-0.00001°
Longitude
-97.40023°
Altitude
506.196 km
Speed
7.613 km/s
True Right ascension
20h 06m 41s
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
08:19:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.889 km
Perigee altitude
507.743 km
Semi-major axis
6,885.953 km
Eccentricity
0.00001
Inclination
45.0029°
RAAN
301.6738°
Arg. of periapsis
77.3968°
True anomaly
282.69122°
Mean anomaly
282.6924°
Eccentric anomaly
282.69181°
Mean motion
3.79837 °/min
Orbital period
94.78 mins
BSTAR
0.00046924
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-06 20:33:12.513Z | 222.479° SW | 2026-02-06 20:37:12.513Z | 128.963° SE | 35.431° | 2026-02-06 20:40:12.513Z | 76.075° E |
| 5 mins | 2026-02-06 22:14:12.513Z | 281.125° WNW | 2026-02-06 22:16:12.513Z | 348.777° N | 37.535° | 2026-02-06 22:19:12.513Z | 59.351° ENE |
| 5 mins | 2026-02-06 23:54:12.513Z | 312.998° NW | 2026-02-06 23:56:12.513Z | 16.6° NNE | 31.659° | 2026-02-06 23:59:12.513Z | 72.807° E |
| 6 mins | 2026-02-07 01:33:12.513Z | 296.246° NW | 2026-02-07 01:35:12.513Z | 319.008° NNW | 43.719° | 2026-02-07 01:39:12.513Z | 111.017° ESE |
| 4 mins | 2026-02-07 03:13:12.513Z | 246.737° WSW | 2026-02-07 03:14:12.513Z | 225.752° WSW | 20.014° | 2026-02-07 03:17:12.513Z | 170.73° S |
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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