Showing default

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.

Loading next visibility...
Identifier
43807, 2018-099BB
Orbit
SSO
Country
Flag of DEDE / GER
Related business
Manufacturer
DLR-ISS
Mission
Operational Civil Science
Bus & Motor
CSBUS, Unknown motor
Mass
250 kg wet, 250 kg dry
Launch date (UTC)
2018-12-03 (7 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 4 Pan, 1.4 m
Radar Cross Section
2.317 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 EUCROPIS
1 43807U 18099BB  26034.58805556  .00008580  00000-0  41904-3 0  9998
2 43807  97.4419  92.4492 0006607  55.0024 305.1830 15.18486361392178
Epoch: 2026-02-03T14:06Z
TLE epoch observation values (Epoch: 2026-02-03T14:06:48.000Z)
Latitude
0.00003°
Longitude
106.98236°
Altitude
510.881 km
Speed
7.61 km/s
True Right ascension
06h 09m 47s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
02:17:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.933 km
Perigee altitude
502.835 km
Semi-major axis
6,885.521 km
Eccentricity
0.00066
Inclination
97.4419°
RAAN
92.4492°
Arg. of periapsis
55.0024°
True anomaly
305.12109°
Mean anomaly
305.183°
Eccentric anomaly
305.15205°
Mean motion
3.79873 °/min
Orbital period
94.77 mins
BSTAR
0.00041904
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|