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: 19 hours ago
TLE from 19 hours ago
0 GITAI-SC1
1 62388U 24247M 25340.86340049 .00009354 00000-0 44183-3 0 9998
2 62388 45.0015 269.9748 0000835 293.8309 66.2484 15.19749372 53465Epoch: 2025-12-06T20:43Z
TLE epoch observation values (Epoch: 2025-12-06T20:43:17.802Z)
Latitude
0.00003°
Longitude
-116.73438°
Altitude
506.365 km
Speed
7.613 km/s
True Right ascension
17h 59m 53s
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
13:33:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.776 km
Perigee altitude
507.626 km
Semi-major axis
6,886.338 km
Eccentricity
0.00008
Inclination
45.0015°
RAAN
269.9748°
Arg. of periapsis
293.8309°
True anomaly
66.25716°
Mean anomaly
66.2484°
Eccentric anomaly
66.25278°
Mean motion
3.79805 °/min
Orbital period
94.79 mins
BSTAR
0.00044183
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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 | 2025-12-07 22:08:58.658Z | 208.059° SW | 2025-12-07 22:11:58.658Z | 146.564° SSE | 29.436° | 2025-12-07 22:14:58.658Z | 83.704° E |
| 6 mins | 2025-12-07 23:48:58.658Z | 268.429° W | 2025-12-07 23:50:58.658Z | 323.314° NNW | 40.427° | 2025-12-07 23:54:58.658Z | 63.077° ENE |
| 5 mins | 2025-12-08 01:28:58.658Z | 306.487° NW | 2025-12-08 01:30:58.658Z | 2.838° NNE | 31.465° | 2025-12-08 01:33:58.658Z | 66.687° ENE |
| 6 mins | 2025-12-08 03:07:58.658Z | 299.865° NW | 2025-12-08 03:10:58.658Z | 53.951° ENE | 41.3° | 2025-12-08 03:13:58.658Z | 101.354° ESE |
| 5 mins | 2025-12-08 04:47:58.658Z | 259.706° W | 2025-12-08 04:49:58.658Z | 209.11° SW | 26.146° | 2025-12-08 04:52:58.658Z | 155.629° 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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