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EUCROPIS

In orbit NORAD 43807 FDMQ-4877-9089-8664-0698 Germany

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
EUCROPIS
Other names
2018-099BB
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2018-12-03 00:00:00
Separation time
2018-12-03 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
494.23 km
Apogee
499.51 km
Inclination
97.4°
Period
94.6 min
Semi-major axis
6875.0 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:55 UTC
Two-line elements (TLE)
1 43807U 18099BB  26283.43523277  .00006730  00000-0  29793-3 0  9992
2 43807 97.4093 337.4937 0003853 243.6387 116.4454 15.21972718429984
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-11 20:11:14 EUCROPIS
NORAD 43807
COSMOS 397 DEB
NORAD 5012
4.746 5.62 1.8e-07
2026-10-13 04:19:05 EUCROPIS
NORAD 43807
OBJECT C
NORAD 61896
3.242 1.77 4.2e-07
2026-10-14 04:58:42 EUCROPIS
NORAD 43807
SPACEMOBILE-004
NORAD 61049
2.200 14.00 4.6e-07
2026-10-14 05:41:00 KANOPUS-V 4
NORAD 43181
EUCROPIS
NORAD 43807
3.782 14.59 1.3e-07
2026-10-14 06:22:27 EUCROPIS
NORAD 43807
CARBSAR
NORAD 67397
4.506 7.10 2.0e-07
2026-10-14 06:54:57 EUCROPIS
NORAD 43807
COSMOS 2251 DEB
NORAD 34856
4.778 15.14 6.7e-08
2026-10-14 07:15:40 KANOPUS-V 4
NORAD 43181
EUCROPIS
NORAD 43807
1.094 14.59 1.6e-06
2026-10-14 08:03:00 KANOPUS-V 4
NORAD 43181
EUCROPIS
NORAD 43807
4.935 14.62 7.7e-08
2026-10-14 08:50:19 KANOPUS-V 4
NORAD 43181
EUCROPIS
NORAD 43807
3.311 14.59 1.7e-07
2026-10-14 09:37:39 KANOPUS-V 4
NORAD 43181
EUCROPIS
NORAD 43807
3.605 14.62 1.4e-07
2026-10-14 11:12:19 KANOPUS-V 4
NORAD 43181
EUCROPIS
NORAD 43807
4.963 14.62 7.6e-08
2026-10-14 15:25:06 CELTEE 1
NORAD 41850
EUCROPIS
NORAD 43807
2.729 15.08 2.1e-07
2026-10-14 16:32:40 EUCROPIS
NORAD 43807
OBJECT B
NORAD 65489
3.238 13.67 2.2e-07
2026-10-14 17:23:48 EUCROPIS
NORAD 43807
SITRO-AIS-57
NORAD 67256
3.749 2.47 3.1e-07
2026-10-15 23:21:21 EUCROPIS
NORAD 43807
OBJECT E
NORAD 67750
3.168 9.07 3.6e-07
2026-10-16 00:21:00 EUCROPIS
NORAD 43807
TOMORROW-S5
NORAD 63234
1.266 14.92 1.0e-06
2026-10-16 13:32:59 EUCROPIS
NORAD 43807
OBJECT C
NORAD 63293
4.432 10.39 1.7e-07
2026-10-16 16:45:08 QB50P1
NORAD 40025
EUCROPIS
NORAD 43807
3.106 4.43 4.4e-07
2026-10-16 19:33:23 EUCROPIS
NORAD 43807
YAOGAN-36 03B
NORAD 54374
2.254 8.17 7.5e-07
2026-10-16 19:53:15 EUCROPIS
NORAD 43807
OBJECT AK
NORAD 67281
2.950 2.43 5.0e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite