Showing default

UMBRA-05, 55036

Orbit data source: Space-Track

UMBRA-05, 55036 is a payload satellite owned by Umbra Labs (US) in SSO 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
SSO
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: 1 day ago

TLE from 1 day ago
0 UMBRA-05
1 55036U 23001AD  25309.12989287  .00422576  00000-0  24729-2 0  9992
2 55036  97.3449   9.7109 0002581 296.5521  63.5481 15.77176495157821
Epoch: 2025-11-05T03:07Z
TLE epoch observation values (Epoch: 2025-11-05T03:07:02.743Z)
Latitude
0.00001°
Longitude
-81.65752°
Altitude
340.842 km
Speed
7.705 km/s
True Right ascension
00h 38m 50s
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
00:44:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
337.065 km
Perigee altitude
333.599 km
Semi-major axis
6,713.469 km
Eccentricity
0.00026
Inclination
97.3449°
RAAN
9.7109°
Arg. of periapsis
296.5521°
True anomaly
63.57458°
Mean anomaly
63.5481°
Eccentric anomaly
63.56134°
Mean motion
3.94569 °/min
Orbital period
91.24 mins
BSTAR
0.0024729
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|