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ESEO

In orbit NORAD 43792 SEXU-2964-9908-3979-4793 ESA Denmark United Kingdom Hungary Italy

Falcon 9

Carrier rocket

База Вандерберг

Spaceport

2

Observations all time

Mission information
Spacecraft name
ESEO
Other names
FunCube 4
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
Spaceport
База Вандерберг
Launch time
2018-12-03 00:00:00
Separation time
Satellite appearance
Operator
ESA
Data for the last 30 days
Orbital parameters of the satellite
Perigee
542.48 km
Apogee
557.51 km
Inclination
97.4°
Period
95.7 min
Semi-major axis
6928.1 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:17 UTC
Two-line elements (TLE)
1 43792U 18099AL  26282.91698232  .00001571  00000-0  11625-3 0  9994
2 43792 97.3863 315.3503 0010845 305.5158 54.5056 15.04510673429055
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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 06:48:48 YAOGAN-30 05A
NORAD 43170
ESEO
NORAD 43792
3.356 13.62 2.1e-07
2026-10-11 12:11:03 ESEO
NORAD 43792
CZ-4B DEB
NORAD 26128
3.303 14.97 1.5e-07
2026-10-12 03:51:41 ESEO
NORAD 43792
CZ-4C DEB
NORAD 43265
1.224 6.61 2.7e-06
2026-10-12 16:35:53 ESEO
NORAD 43792
DMSP 5D-2 F11 DEB
NORAD 29070
3.597 12.22 2.2e-07
2026-10-13 11:00:39 ESEO
NORAD 43792
OKEAN-3
NORAD 21397
4.157 15.06 1.2e-06
2026-10-13 11:48:34 ESEO
NORAD 43792
OKEAN-3
NORAD 21397
3.841 15.06 1.4e-06
2026-10-13 12:36:23 ESEO
NORAD 43792
OKEAN-3
NORAD 21397
4.659 15.06 9.3e-07
2026-10-13 13:24:18 ESEO
NORAD 43792
OKEAN-3
NORAD 21397
4.790 15.06 8.8e-07
2026-10-13 18:13:28 ESEO
NORAD 43792
IRIDIUM 33 DEB
NORAD 36028
4.676 14.86 7.7e-08
2026-10-15 05:41:51 YAOGAN-30 05B
NORAD 43171
ESEO
NORAD 43792
3.993 13.88 1.4e-07
2026-10-15 11:40:29 ESEO
NORAD 43792
JILIN GAOFEN OBJECT D
NORAD 68694
3.251 5.53 3.9e-07
2026-10-15 12:27:22 ESEO
NORAD 43792
METOP-A
NORAD 29499
1.723 9.52 1.2e-06
2026-10-16 04:24:37 COSMOS 2493 (SKRL-756 1)
NORAD 39490
ESEO
NORAD 43792
2.291 15.16 2.8e-07
2026-10-16 06:00:27 COSMOS 2493 (SKRL-756 1)
NORAD 39490
ESEO
NORAD 43792
1.450 15.16 7.0e-07
2026-10-16 06:48:15 ESEO
NORAD 43792
CZ-6A DEB
NORAD 54523
4.763 10.79 1.4e-07
2026-10-16 07:36:17 COSMOS 2493 (SKRL-756 1)
NORAD 39490
ESEO
NORAD 43792
3.922 15.16 9.6e-08
2026-10-16 18:41:56 SNAP-3 JIMI
NORAD 40975
ESEO
NORAD 43792
4.003 13.55 1.5e-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