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UMBRA-05, 55036

Orbit data source: Space-Track

UMBRA-05, 55036 is a payload satellite owned by Umbra Labs (US) in LEO that was launched on Tue, 03 Jan 2023 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

Not visible in the next 10 days
Identifier
55036, 2023-001AD
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
Umbra Labs
Mission
Operational Commercial Radar Imaging
Bus & Motor
UMBRA, Unknown motor
Mass
65 kg wet, 60 kg dry
Launch date (UTC)
2023-01-03 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan + 1 Dish, 2.0 m
Radar Cross Section
6.513 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 weeks ago

TLE from 3 weeks ago
0 UMBRA-05
1 55036U 23001AD  25322.64617760  .12960904  24647-5  24517-2 0  9996
2 55036  97.3289  24.3388 0010620 263.3772  96.6315 16.31913080159979
Epoch: 2025-11-18T15:30Z
TLE epoch observation values (Epoch: 2025-11-18T15:30:29.744Z)
Latitude
Longitude
93.78559°
Altitude
191.459 km
Speed
7.791 km/s
True Right ascension
01h 37m 21s
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
05:25:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
191.188 km
Perigee altitude
177.249 km
Semi-major axis
6,562.356 km
Eccentricity
0.00106
Inclination
97.3289°
RAAN
24.3388°
Arg. of periapsis
263.3772°
True anomaly
96.75236°
Mean anomaly
96.6315°
Eccentric anomaly
96.69193°
Mean motion
4.08276 °/min
Orbital period
88.18 mins
BSTAR
0.0024517
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Computing Atmospheric mass density...

Documentation

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