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: 6 days ago
TLE from 6 days ago
0 ORBITER SN3
1 56960U 23084AE 26155.28208348 .00009183 00000-0 27754-3 0 9996
2 56960 97.6262 295.6726 0008234 27.6644 332.5035 15.34436786165519Epoch: 2026-06-04T06:46Z
TLE epoch observation values (Epoch: 2026-06-04T06:46:12.012Z)
Latitude
-0.00002°
Longitude
-58.60604°
Altitude
460.701 km
Speed
7.639 km/s
True Right ascension
19h 42m 41s
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
14:06:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
465.18 km
Perigee altitude
453.92 km
Semi-major axis
6,837.687 km
Eccentricity
0.00082
Inclination
97.6262°
RAAN
295.6726°
Arg. of periapsis
27.6644°
True anomaly
332.4599°
Mean anomaly
332.5035°
Eccentric anomaly
332.4817°
Mean motion
3.83866 °/min
Orbital period
93.78 mins
BSTAR
0.00027754
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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 | 2026-06-10 10:01:16.941Z | 214.822° SW | 2026-06-10 10:03:16.941Z | 265.894° W | 24.469° | 2026-06-10 10:05:16.941Z | 313.537° NW |
| 4 mins | 2026-06-10 22:58:16.941Z | 330.855° NNW | 2026-06-10 23:00:16.941Z | 281.793° WNW | 22.04° | 2026-06-10 23:02:16.941Z | 240.348° WSW |
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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