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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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Identifier
56933, 2023-084B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Starfish Space
Mission
Partially operational Commercial Technology
Bus & Motor
OTTER, EP
Mass
~50 kg wet, 50 kg dry
Launch date (UTC)
2023-06-12 (3 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 OTTER PUP
1 56933U 23084B   26039.37328266  .00114549  00000-0  79315-3 0  9992
2 56933  97.5771 192.4508 0003153 314.7762  45.3245 15.74148764148873
Epoch: 2026-02-08T08:57Z
TLE epoch observation values (Epoch: 2026-02-08T08:57:31.621Z)
Latitude
-0.00004°
Longitude
-80.41433°
Altitude
348.722 km
Speed
7.701 km/s
True Right ascension
12h 49m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:28:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
346.076 km
Perigee altitude
341.837 km
Semi-major axis
6,722.093 km
Eccentricity
0.00032
Inclination
97.5771°
RAAN
192.4508°
Arg. of periapsis
314.7762°
True anomaly
45.3502°
Mean anomaly
45.3245°
Eccentric anomaly
45.33735°
Mean motion
3.9381 °/min
Orbital period
91.41 mins
BSTAR
0.00079315
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