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: 7 hours ago
TLE from 7 hours ago
0 GITAI-SC1
1 62388U 24247M 26296.10903747 .00005569 00000-0 24802-3 0 9996
2 62388 45.0000 339.3514 0001543 325.3793 34.6987 15.22466947102221Epoch: 2026-10-23T02:37Z
TLE epoch observation values (Epoch: 2026-10-23T02:37:00.837Z)
Latitude
-0.00005°
Longitude
-91.43644°
Altitude
497.529 km
Speed
7.618 km/s
True Right ascension
22h 37m 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
04:53:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
501.069 km
Perigee altitude
498.947 km
Semi-major axis
6,878.145 km
Eccentricity
0.00015
Inclination
45°
RAAN
339.3514°
Arg. of periapsis
325.3793°
True anomaly
34.70877°
Mean anomaly
34.6987°
Eccentric anomaly
34.70373°
Mean motion
3.80484 °/min
Orbital period
94.62 mins
BSTAR
0.00024802
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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 | 2026-10-23 10:54:10.892Z | 297.889° NW | 2026-10-23 10:58:10.892Z | 47.155° ENE | 53.98° | 2026-10-23 11:01:10.892Z | 96.302° ESE |
| 5 mins | 2026-10-23 12:35:10.892Z | 261.392° W | 2026-10-23 12:37:10.892Z | 200.225° SSW | 34.781° | 2026-10-23 12:40:10.892Z | 148.095° SSE |
| 5 mins | 2026-10-24 05:35:10.892Z | 191.861° SSW | 2026-10-24 05:37:10.892Z | 142.681° SSE | 30.266° | 2026-10-24 05:40:10.892Z | 84.835° E |
| 5 mins | 2026-10-24 07:14:10.892Z | 266.6° W | 2026-10-24 07:16:10.892Z | 349.72° N | 63.787° | 2026-10-24 07:19:10.892Z | 61.248° ENE |
| 6 mins | 2026-10-24 08:53:10.892Z | 299.38° NW | 2026-10-24 08:55:10.892Z | 342.592° N | 35.783° | 2026-10-24 08:59:10.892Z | 68.233° E |
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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