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). Payloads include a variety of satellites, spacecraft, and rockets 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)
ORBITER SN3 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 6 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl, 1 m |
| Radar Cross Section | 0.583 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 6 hours ago
0 ORBITER SN3
1 56960U 23084AE 24326.13344631 .00010982 00000-0 47640-3 0 9999
2 56960 97.5612 84.6118 0010289 190.8049 169.2967 15.22479710 79933Epoch: 2024-11-21T03:12Z
Definitive object data (Epoch: 2024-11-21T03:12:09.761Z)
| Latitude | -0.00007° |
| Longitude | -24.04842° |
| Altitude | 508.407 km |
| Speed | 7.606 km/s |
| True Right ascension | 05h 38m 26s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 33.32187° |
| Longitude | -28.75653° |
| Altitude | 509.283 km |
| Speed | 7.609 km/s |
| Apparent Right ascension | 01h 36m 25s |
| Apparent Declination | -8° 19' 46" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 06:42:36 |
| Azimuth | 254.947° W |
| Elevation | 4.795° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 502.405 km |
| Perigee altitude | 488.261 km |
| Semi-major axis | 6,873.47 km |
| Eccentricity | 0.0010289 |
| Inclination | 97.5612° |
| RAAN | 84.6118° |
| Arg. of periapsis | 190.8049° |
| True anomaly | 169.31857° |
| Mean anomaly | 169.2967° |
| Eccentric anomaly | 169.30764° |
| Mean motion | 3.80872 °/min |
| BSTAR | 0.0004764 |
| Orbital period | 94.52 mins |
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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)
ORBITER SN3 Visibility forecast
Observer location: undefined°, undefined
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 | 2024-11-21 21:06:32.922Z | 6.782° NNE | 2024-11-21 21:09:32.922Z | 321.822° NNW | 42.233° | 2024-11-21 21:12:32.922Z | 202.431° SSW |
| 5 mins | 2024-11-22 07:44:32.922Z | 133.368° SE | 2024-11-22 07:46:32.922Z | 77.162° E | 33.342° | 2024-11-22 07:49:32.922Z | 5.851° NNE |
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