EUCROPIS, 43807
Orbit data source: Space-Track
EUCROPIS, 43807 is a payload satellite owned by DLR (DE) in SSO that was launched on Mon, 03 Dec 2018 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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43807 intel report (Beta)
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Identifier
Orbit
Country
DE / GERRelated business
Manufacturer
DLR-ISS
Mission
Operational Civil Science
Bus & Motor
CSBUS, Unknown motor
Mass
250 kg wet, 250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 4 Pan, 1.5 m
Radar Cross Section
2.317 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 EUCROPIS
1 43807U 18099BB 26295.72899172 .00007642 00000-0 33597-3 0 9997
2 43807 97.4079 349.6024 0004914 193.6194 166.4911 15.22160876431856Epoch: 2026-10-22T17:29Z
TLE epoch observation values (Epoch: 2026-10-22T17:29:44.884Z)
Latitude
0.00002°
Longitude
56.00567°
Altitude
505.704 km
Speed
7.609 km/s
True Right ascension
23h 18m 24s
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
06:14:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.665 km
Perigee altitude
492.909 km
Semi-major axis
6,874.424 km
Eccentricity
0.00049
Inclination
97.4079°
RAAN
349.6024°
Arg. of periapsis
193.6194°
True anomaly
166.50425°
Mean anomaly
166.4911°
Eccentric anomaly
166.49767°
Mean motion
3.80793 °/min
Orbital period
94.54 mins
BSTAR
0.00033597
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Other satellites on launch #99 in the year 2018 (2018-12-03 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.EUCROPIS 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-10-23 16:09:25.225Z | 35.076° NE | 2026-10-23 16:12:25.225Z | 115.484° SE | 36.078° | 2026-10-23 16:14:25.225Z | 159.688° S |
| 5 mins | 2026-10-24 04:20:25.225Z | 209.566° SW | 2026-10-24 04:22:25.225Z | 256.977° W | 31.376° | 2026-10-24 04:25:25.225Z | 323.237° NNW |
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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