ORBITER SN3, 56960
Orbit data source: Space-Track
ORBITER SN3, 56960 is a payload satellite owned by Launcher Inc (US) 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.
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56960 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Launcher Inc
Mission
Operational Commercial Technology
Bus & Motor
LAORB1, AOCS
Mass
223 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: 13 hours ago
TLE from 13 hours ago
0 ORBITER SN3
1 56960U 23084AE 26034.62337646 .00010415 00000-0 33700-3 0 9992
2 56960 97.6052 171.3763 0009605 87.3523 272.8818 15.32207437147027Epoch: 2026-02-03T14:57Z
TLE epoch observation values (Epoch: 2026-02-03T14:57:39.726Z)
Latitude
0.00005°
Longitude
173.15912°
Altitude
472.004 km
Speed
7.63 km/s
True Right ascension
11h 25m 30s
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
05:39:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
472.76 km
Perigee altitude
459.612 km
Semi-major axis
6,844.323 km
Eccentricity
0.00096
Inclination
97.6052°
RAAN
171.3763°
Arg. of periapsis
87.3523°
True anomaly
272.77187°
Mean anomaly
272.8818°
Eccentric anomaly
272.82683°
Mean motion
3.83308 °/min
Orbital period
93.92 mins
BSTAR
0.000337
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.ORBITER SN3 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-04 08:20:58.451Z | 118.29° SE | 2026-02-04 08:22:58.451Z | 76.999° E | 21.37° | 2026-02-04 08:24:58.451Z | 29.305° NE |
| 4 mins | 2026-02-04 21:19:58.451Z | 62.781° ENE | 2026-02-04 21:20:58.451Z | 91.112° ESE | 24.705° | 2026-02-04 21:23:58.451Z | 156.075° SSE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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