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GEISAT PRECURSOR, 56934

Orbit data source: Space-Track

GEISAT PRECURSOR, 56934 is a payload satellite owned by Satlantis (ES) in SSO that was launched on Mon, 12 Jun 2023 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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Identifier
56934, 2023-084C
Orbit
SSO
Country
Flag of ESES / SPN
Related business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U M16P, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
2023-06-12 (2 years 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: 10 hours ago

TLE from 10 hours ago
0 GEISAT PRECURSOR
1 56934U 23084C   25286.59906122  .00011181  00000-0  38754-3 0  9993
2 56934  97.5924  55.8007 0007599 132.8745 227.3134 15.29976750129768
Epoch: 2025-10-13T14:22Z
TLE epoch observation values (Epoch: 2025-10-13T14:22:38.889Z)
Latitude
-0.00005°
Longitude
177.73914°
Altitude
482.514 km
Speed
7.622 km/s
True Right ascension
03h 43m 12s
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
19:19:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.048 km
Perigee altitude
467.636 km
Semi-major axis
6,850.979 km
Eccentricity
0.00076
Inclination
97.5924°
RAAN
55.8007°
Arg. of periapsis
132.8745°
True anomaly
227.24943°
Mean anomaly
227.3134°
Eccentric anomaly
227.28141°
Mean motion
3.82749 °/min
Orbital period
94.06 mins
BSTAR
0.00038754
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