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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Edit Public Description
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, 1.4 m
Radar Cross Section
2.317 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 EUCROPIS
1 43807U 18099BB 25286.15798590 .00013873 00000-0 72352-3 0 9990
2 43807 97.4592 340.8985 0007425 83.8976 276.3103 15.16047308374973Epoch: 2025-10-13T03:47Z
TLE epoch observation values (Epoch: 2025-10-13T03:47:29.981Z)
Latitude
-0.00001°
Longitude
-97.94121°
Altitude
520.325 km
Speed
7.604 km/s
True Right ascension
22h 43m 35s
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
11:56:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.892 km
Perigee altitude
509.656 km
Semi-major axis
6,892.911 km
Eccentricity
0.00074
Inclination
97.4592°
RAAN
340.8985°
Arg. of periapsis
83.8976°
True anomaly
276.22572°
Mean anomaly
276.3103°
Eccentric anomaly
276.26801°
Mean motion
3.79262 °/min
Orbital period
94.92 mins
BSTAR
0.00072352
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-14 03:40:53.897Z | 158.996° S | 2025-10-14 03:43:53.897Z | 67.088° ENE | 43.554° | 2025-10-14 03:46:53.897Z | 353.389° N |
| 5 mins | 2025-10-14 16:47:53.897Z | 2.822° NNE | 2025-10-14 16:49:53.897Z | 317.058° NNW | 42.13° | 2025-10-14 16:52:53.897Z | 203.47° SW |
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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