EIVE, 56937 (Decayed)
Orbit data source: Space-Track
EIVE, 56937 was a payload satellite owned by IRS Stuttgart (DE) in LEO 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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56937 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
IRS Stuttgart
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 6 months ago
TLE from 6 months ago
0 EIVE
1 56937U 23084F 25099.34660221 .07763351 25571-5 18278-2 0 9991
2 56937 97.5157 237.0989 0012765 277.1321 82.8521 16.29514234101968Epoch: 2025-04-09T08:19Z
TLE epoch observation values (Epoch: 2025-04-09T08:19:06.430Z)
Latitude
-0.00005°
Longitude
-85.51252°
Altitude
196.046 km
Speed
7.789 km/s
True Right ascension
15h 48m 23s
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
14:41:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
199.057 km
Perigee altitude
182.287 km
Semi-major axis
6,568.809 km
Eccentricity
0.00128
Inclination
97.5157°
RAAN
237.0989°
Arg. of periapsis
277.1321°
True anomaly
82.99727°
Mean anomaly
82.8521°
Eccentric anomaly
82.92468°
Mean motion
4.07674 °/min
Orbital period
88.31 mins
BSTAR
0.0018278
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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.EIVE Visibility
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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. |
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| This satellite is decayed. |
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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