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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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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ORBITER SN3
1 56960U 23084AE 26308.94788572 .00007306 00000-0 20720-3 0 9992
2 56960 97.6454 94.8803 0007364 180.9755 179.1475 15.36531060189091Epoch: 2026-11-04T22:44Z
TLE epoch observation values (Epoch: 2026-11-04T22:44:57.326Z)
Latitude
-0.00004°
Longitude
69.45256°
Altitude
464.516 km
Speed
7.631 km/s
True Right ascension
06h 19m 31s
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
18:24:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.362 km
Perigee altitude
448.3 km
Semi-major axis
6,831.468 km
Eccentricity
0.00074
Inclination
97.6454°
RAAN
94.8803°
Arg. of periapsis
180.9755°
True anomaly
179.14875°
Mean anomaly
179.1475°
Eccentric anomaly
179.14813°
Mean motion
3.8439 °/min
Orbital period
93.65 mins
BSTAR
0.0002072
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-05 22:44:43.946Z | 12.929° NNE | 2026-11-05 22:47:43.946Z | 23.19° NE | 73.793° | 2026-11-05 22:50:43.946Z | 191.89° SSW |
| 4 mins | 2026-11-06 09:17:43.946Z | 106.317° ESE | 2026-11-06 09:18:43.946Z | 80.89° E | 24.971° | 2026-11-06 09:21:43.946Z | 15.984° NNE |
| 4 mins | 2026-11-06 22:13:43.946Z | 61.295° ENE | 2026-11-06 22:14:43.946Z | 89.904° E | 27.685° | 2026-11-06 22:17:43.946Z | 156.767° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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