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). 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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56933 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
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
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
1.500 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 OTTER PUP
1 56933U 23084B 25306.34739201 .00049071 00000-0 66709-3 0 9990
2 56933 97.5818 87.0517 0003150 339.9934 20.1196 15.57447693133549Epoch: 2025-11-02T08:20Z
TLE epoch observation values (Epoch: 2025-11-02T08:20:14.669Z)
Latitude
-0.00012°
Longitude
-79.87383°
Altitude
396.179 km
Speed
7.674 km/s
True Right ascension
05h 48m 12s
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
15:46:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
394.103 km
Perigee altitude
389.838 km
Semi-major axis
6,770.108 km
Eccentricity
0.00032
Inclination
97.5818°
RAAN
87.0517°
Arg. of periapsis
339.9934°
True anomaly
20.13202°
Mean anomaly
20.1196°
Eccentric anomaly
20.12581°
Mean motion
3.89628 °/min
Orbital period
92.4 mins
BSTAR
0.00066709
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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.OTTER PUP 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 | 2025-11-03 21:54:55.409Z | 46.642° ENE | 2025-11-03 21:56:55.409Z | 105.045° ESE | 24.941° | 2025-11-03 21:58:55.409Z | 154.28° 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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