DECAYED
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ORBITERSN1, 55059 (Decayed)

Orbit data source: Space-Track

ORBITERSN1, 55059 was a payload satellite owned by Launcher Inc (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
55059, 2023-001BC
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
Launcher Inc
Mission
Decayed Commercial Technology
Bus & Motor
LAORB1, AOCS
Mass
~200 kg wet, ~150 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
Oct Cyl, 0.5 m
Radar Cross Section
0.583 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 year ago

TLE from 1 year ago
0 ORBITERSN1
1 55059U 23001BC  25002.46364407  .13531508  25299-5  55012-3 0  9997
2 55059  97.3687  78.2320 0010778 277.4611  82.5465 16.42795588111805
Epoch: 2025-01-02T11:07Z
TLE epoch observation values (Epoch: 2025-01-02T11:07:38.847Z)
Latitude
-0.00006°
Longitude
168.97794°
Altitude
160.726 km
Speed
7.81 km/s
True Right ascension
05h 12m 55s
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
03:57:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.221 km
Perigee altitude
148.137 km
Semi-major axis
6,533.316 km
Eccentricity
0.00108
Inclination
97.3687°
RAAN
78.232°
Arg. of periapsis
277.4611°
True anomaly
82.66898°
Mean anomaly
82.5465°
Eccentric anomaly
82.60774°
Mean motion
4.11001 °/min
Orbital period
87.59 mins
BSTAR
0.00055012
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