OTTER PUP, 56933
Orbit data source: Space-Track
OTTER PUP, 56933 is a payload satellite owned by Starfish Space (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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Edit Public Description
| Identifier | |
| Orbit | SSO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | Starfish Space |
| Mission | Partially operational Commercial Technology |
| Bus & Motor | OTTER, EP |
| Mass | ~50 kg wet, 50 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 1 m |
| Radar Cross Section | 1.500 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 OTTER PUP
1 56933U 23084B 25070.80607437 .00035414 00000-0 89031-3 0 9993
2 56933 97.5539 200.4434 0005290 127.2180 232.9549 15.39866119 97100Epoch: 2025-03-11T19:20Z
Definitive object data (Epoch: 2025-03-11T19:20:44.825Z)
| Latitude | -0.00002° |
| Longitude | 100.55289° |
| Altitude | 451.794 km |
| Speed | 7.64 km/s |
| True Right ascension | 13h 21m 46s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -60.96531° |
| Longitude | -92.7431° |
| Altitude | 471.502 km |
| Speed | 7.628 km/s |
| Apparent Right ascension | 23h 02m 41s |
| Apparent Declination | -51° 59' 10" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 10:04:59 |
| Azimuth | 214.694° SW |
| Elevation | -74.367° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 447.059 km |
| Perigee altitude | 439.842 km |
| Semi-major axis | 6,821.588 km |
| Eccentricity | 0.000529 |
| Inclination | 97.5539° |
| RAAN | 200.4434° |
| Arg. of periapsis | 127.218° |
| True anomaly | 232.90654° |
| Mean anomaly | 232.9549° |
| Eccentric anomaly | 232.93072° |
| Mean motion | 3.85225 °/min |
| BSTAR | 0.00089031 |
| Orbital period | 93.45 mins |
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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)
OTTER PUP 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-03-12 07:57:56.899Z | 123.643° SE | 2025-03-12 07:59:56.899Z | 82.351° E | 22.657° | 2025-03-12 08:02:56.899Z | 15.746° NNE |
| 4 mins | 2025-03-12 20:52:56.899Z | 55.083° ENE | 2025-03-12 20:54:56.899Z | 113.185° SE | 23.615° | 2025-03-12 20:56:56.899Z | 153.485° SSE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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