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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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: 12 hours ago
TLE from 12 hours ago
0 OTTER PUP
1 56933U 23084B 26079.91362558 .00222799 00000-0 86013-3 0 9998
2 56933 97.5758 236.9899 0003527 235.3522 124.7416 15.86702698155271Epoch: 2026-03-20T21:55Z
TLE epoch observation values (Epoch: 2026-03-20T21:55:37.250Z)
Latitude
-0.00003°
Longitude
89.64283°
Altitude
316.055 km
Speed
7.718 km/s
True Right ascension
15h 47m 57s
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
14:39:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
310.778 km
Perigee altitude
306.061 km
Semi-major axis
6,686.557 km
Eccentricity
0.00035
Inclination
97.5758°
RAAN
236.9899°
Arg. of periapsis
235.3522°
True anomaly
124.7748°
Mean anomaly
124.7416°
Eccentric anomaly
124.7582°
Mean motion
3.96953 °/min
Orbital period
90.69 mins
BSTAR
0.00086013
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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 | 2026-03-21 10:10:22.985Z | 143.323° SSE | 2026-03-21 10:12:22.985Z | 78.804° E | 32.229° | 2026-03-21 10:14:22.985Z | 7.211° NNE |
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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