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: 2 days ago
TLE from 2 days ago
0 GITAI-SC1
1 62388U 24247M 25344.14999254 .00008017 00000-0 38099-3 0 9995
2 62388 45.0004 252.2472 0001048 295.6897 64.3874 15.19705760 53961Epoch: 2025-12-10T03:35Z
TLE epoch observation values (Epoch: 2025-12-10T03:35:59.355Z)
Latitude
-0.00007°
Longitude
119.12536°
Altitude
506.416 km
Speed
7.613 km/s
True Right ascension
16h 48m 59s
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
14:01:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.055 km
Perigee altitude
507.611 km
Semi-major axis
6,886.47 km
Eccentricity
0.0001
Inclination
45.0004°
RAAN
252.2472°
Arg. of periapsis
295.6897°
True anomaly
64.39823°
Mean anomaly
64.3874°
Eccentric anomaly
64.39281°
Mean motion
3.79794 °/min
Orbital period
94.79 mins
BSTAR
0.00038099
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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 | 2025-12-11 20:49:10.002Z | 220.089° SW | 2025-12-11 20:52:10.002Z | 149.187° SSE | 36.658° | 2025-12-11 20:55:10.002Z | 77.752° E |
| 6 mins | 2025-12-11 22:29:10.002Z | 277.596° WNW | 2025-12-11 22:31:10.002Z | 325.902° NNW | 36.625° | 2025-12-11 22:35:10.002Z | 62.221° ENE |
| 5 mins | 2025-12-12 00:09:10.002Z | 307.13° NW | 2025-12-12 00:11:10.002Z | 359.745° N | 32.078° | 2025-12-12 00:14:10.002Z | 70.127° E |
| 6 mins | 2025-12-12 01:48:10.002Z | 295.291° NW | 2025-12-12 01:51:10.002Z | 86.36° E | 44.098° | 2025-12-12 01:54:10.002Z | 111.237° ESE |
| 4 mins | 2025-12-12 03:28:10.002Z | 253.661° W | 2025-12-12 03:30:10.002Z | 212.562° SW | 19.763° | 2025-12-12 03:32:10.002Z | 176.255° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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