Showing default

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.

Loading next visibility...
Identifier
62388, 2024-247M
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
GITAI USA
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 16U, Unknown motor
Mass
20 kg wet, 20 kg dry
Launch date (UTC)
2024-12-21 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago
0 GITAI-SC1
1 62388U 24247M   26171.39878977  .00004874  00000-0  22531-3 0  9990
2 62388  45.0009 294.2737 0001360 279.6852  80.3875 15.21417436 83220
Epoch: 2026-06-20T09:34Z
TLE epoch observation values (Epoch: 2026-06-20T09:34:15.436Z)
Latitude
-0°
Longitude
-117.9046°
Altitude
501.407 km
Speed
7.615 km/s
True Right ascension
19h 37m 05s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:18:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.105 km
Perigee altitude
502.233 km
Semi-major axis
6,881.306 km
Eccentricity
0.00014
Inclination
45.0009°
RAAN
294.2737°
Arg. of periapsis
279.6852°
True anomaly
80.40287°
Mean anomaly
80.3875°
Eccentric anomaly
80.39518°
Mean motion
3.80222 °/min
Orbital period
94.68 mins
BSTAR
0.00022531
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|