Showing default

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.

Loading next visibility...
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 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 1.0 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 GEISAT PRECURSOR
1 56934U 23084C   26308.91388922  .00005597  00000-0  16030-3 0  9994
2 56934  97.6401  94.8676 0005180 187.3126 172.8043 15.36349783189123
Epoch: 2026-11-04T21:56Z
TLE epoch observation values (Epoch: 2026-11-04T21:56:00.028Z)
Latitude
0.00001°
Longitude
81.71211°
Altitude
463.533 km
Speed
7.633 km/s
True Right ascension
06h 19m 28s
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
17:18:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
457.407 km
Perigee altitude
450.33 km
Semi-major axis
6,832.006 km
Eccentricity
0.00052
Inclination
97.6401°
RAAN
94.8676°
Arg. of periapsis
187.3126°
True anomaly
172.81173°
Mean anomaly
172.8043°
Eccentric anomaly
172.80802°
Mean motion
3.84345 °/min
Orbital period
93.67 mins
BSTAR
0.0001603
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|