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: 8 hours ago
TLE from 8 hours ago
0 OTTER PUP
1 56933U 23084B 25300.17796255 .00051035 00000-0 71274-3 0 9993
2 56933 97.5819 80.4949 0003209 5.7823 354.3468 15.56711679132580Epoch: 2025-10-27T04:16Z
TLE epoch observation values (Epoch: 2025-10-27T04:16:15.964Z)
Latitude
-0°
Longitude
-19.35516°
Altitude
398.152 km
Speed
7.673 km/s
True Right ascension
05h 21m 58s
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
08:08:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
396.28 km
Perigee altitude
391.933 km
Semi-major axis
6,772.243 km
Eccentricity
0.00032
Inclination
97.5819°
RAAN
80.4949°
Arg. of periapsis
5.7823°
True anomaly
354.34318°
Mean anomaly
354.3468°
Eccentric anomaly
354.34499°
Mean motion
3.89443 °/min
Orbital period
92.44 mins
BSTAR
0.00071274
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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 | 2025-10-27 21:48:46.155Z | 49.192° ENE | 2025-10-27 21:50:46.155Z | 102.909° ESE | 22.538° | 2025-10-27 21:52:46.155Z | 150.051° SSE |
| 4 mins | 2025-10-28 09:43:46.155Z | 190.129° SSW | 2025-10-28 09:44:46.155Z | 225.189° WSW | 38.565° | 2025-10-28 09:47:46.155Z | 338.347° N |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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