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: 10 hours ago
TLE from 10 hours ago
0 ORBITER SN3
1 56960U 23084AE 26316.43673675 .00010158 00000-0 28555-3 0 9995
2 56960 97.6471 102.6652 0007875 155.1098 205.0527 15.36687722190244Epoch: 2026-11-12T10:28Z
TLE epoch observation values (Epoch: 2026-11-12T10:28:54.055Z)
Latitude
0.00002°
Longitude
-106.13028°
Altitude
463.895 km
Speed
7.632 km/s
True Right ascension
06h 50m 39s
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
17:03:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
458.246 km
Perigee altitude
447.487 km
Semi-major axis
6,831.003 km
Eccentricity
0.00079
Inclination
97.6471°
RAAN
102.6652°
Arg. of periapsis
155.1098°
True anomaly
205.01452°
Mean anomaly
205.0527°
Eccentric anomaly
205.03361°
Mean motion
3.84429 °/min
Orbital period
93.65 mins
BSTAR
0.00028555
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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 | 2026-11-12 21:59:40.557Z | 50.142° ENE | 2026-11-12 22:01:40.557Z | 86.917° E | 18.164° | 2026-11-12 22:03:40.557Z | 130.18° SE |
| 5 mins | 2026-11-13 10:03:40.557Z | 176.202° S | 2026-11-13 10:05:40.557Z | 234.182° WSW | 71.018° | 2026-11-13 10:08:40.557Z | 342.554° N |
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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