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: 8 hours ago
TLE from 8 hours ago
0 EUCROPIS
1 43807U 18099BB 26220.10732125 .00004186 00000-0 19024-3 0 9990
2 43807 97.4189 275.1044 0007234 112.7273 247.4728 15.21281464420356Epoch: 2026-08-08T02:34Z
TLE epoch observation values (Epoch: 2026-08-08T02:34:32.555Z)
Latitude
-0.00006°
Longitude
-80.15465°
Altitude
506.976 km
Speed
7.61 km/s
True Right ascension
18h 20m 25s
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
01:06:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.914 km
Perigee altitude
493.964 km
Semi-major axis
6,877.076 km
Eccentricity
0.00072
Inclination
97.4189°
RAAN
275.1044°
Arg. of periapsis
112.7273°
True anomaly
247.39626°
Mean anomaly
247.4728°
Eccentric anomaly
247.43453°
Mean motion
3.80573 °/min
Orbital period
94.59 mins
BSTAR
0.00019024
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-08-08 15:47:20.998Z | 55.419° ENE | 2026-08-08 15:49:20.998Z | 94.712° ESE | 18.446° | 2026-08-08 15:51:20.998Z | 133.946° SE |
| 4 mins | 2026-08-08 17:21:20.998Z | 328.811° NNW | 2026-08-08 17:23:20.998Z | 282.273° WNW | 21.724° | 2026-08-08 17:25:20.998Z | 242.548° WSW |
| 5 mins | 2026-08-09 03:58:20.998Z | 183.184° SSW | 2026-08-09 04:00:20.998Z | 245.469° WSW | 41.561° | 2026-08-09 04:03:20.998Z | 339.066° N |
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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