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, 1.4 m
Radar Cross Section
2.317 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 EUCROPIS
1 43807U 18099BB 26183.13530948 .00009345 00000-0 42674-3 0 9999
2 43807 97.4209 238.6795 0004233 229.2592 130.8276 15.20800331414737Epoch: 2026-07-02T03:14Z
TLE epoch observation values (Epoch: 2026-07-02T03:14:50.739Z)
Latitude
-0.00004°
Longitude
-90.21396°
Altitude
508.422 km
Speed
7.609 km/s
True Right ascension
15h 54m 43s
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
00:26:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.302 km
Perigee altitude
497.479 km
Semi-major axis
6,878.528 km
Eccentricity
0.00042
Inclination
97.4209°
RAAN
238.6795°
Arg. of periapsis
229.2592°
True anomaly
130.86429°
Mean anomaly
130.8276°
Eccentric anomaly
130.84595°
Mean motion
3.80452 °/min
Orbital period
94.62 mins
BSTAR
0.00042674
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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 | 2026-07-04 15:49:29.726Z | 44.12° NE | 2026-07-04 15:52:29.726Z | 99.583° ESE | 19.896° | 2026-07-04 15:54:29.726Z | 138.565° SSE |
| 4 mins | 2026-07-04 17:24:29.726Z | 324.333° NNW | 2026-07-04 17:26:29.726Z | 278.482° WNW | 20.249° | 2026-07-04 17:28:29.726Z | 242.53° WSW |
| 5 mins | 2026-07-05 04:01:29.726Z | 187.679° SSW | 2026-07-05 04:03:29.726Z | 251.274° W | 39.963° | 2026-07-05 04:06:29.726Z | 336.787° 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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