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.
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55059 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Launcher Inc
Mission
Decayed Commercial Technology
Bus & Motor
LAORB1, AOCS
Mass
~200 kg wet, ~150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Oct Cyl, 0.5 m
Radar Cross Section
0.583 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months 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 16.42795588111805Epoch: 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
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:34:32
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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Other satellites on launch #1 in the year 2023 (2023-01-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ORBITERSN1 Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| This satellite is decayed. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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