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ROBUSTA-3A

In orbit NORAD 60243 AEYC-6866-6455-5236-7157 France

Time in UTC

—

No observations scheduled

3

Observations over 30 days

47%

Successful observations

119k

Frames, latest 2026-10-10 15:57 UTC

Mission information
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2024-07-09 19:00:00
Separation time
2024-07-09 20:05:53
Last observers
Observer
Time of receipt
2026-10-09 12:52:43 UTC
2026-10-09 12:52:13 UTC
2026-08-18 07:37:25 UTC
2026-08-17 07:54:49 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
508.99 km
Apogee
543.13 km
Inclination
62.0°
Period
95.2 min
Semi-major axis
6904.2 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:38 UTC
Two-line elements (TLE)
1 60243U 24128J   26283.90701852  .00009028  00000-0  51734-3 0  9997
2 60243 61.9855 158.5920 0024728 151.0327 209.2148 15.12974534123927
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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
2026-10-13 02:52:31 SDGSAT 1
NORAD 49387
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
2.334 14.97 3.0e-07
2026-10-13 17:00:04 PROPCUBE 1 (FLORA)
NORAD 40976
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
3.727 12.80 2.0e-07
2026-10-13 19:57:36 ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
SCOUT X-4 DEB
NORAD 3750
4.617 8.40 1.8e-07
2026-10-14 14:50:47 NANOFF B
NORAD 58755
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
4.076 14.55 1.1e-07
2026-10-14 14:50:48 NANOFF A
NORAD 58810
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
4.422 14.56 9.7e-08
2026-10-14 15:06:55 ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
HULIANWANG JISHU SHIYAN 6C
NORAD 63430
4.806 8.41 1.6e-07
2026-10-14 17:13:31 NANOFF B
NORAD 58755
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
4.023 14.53 1.2e-07
2026-10-14 18:48:45 NANOFF A
NORAD 58810
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
2.008 14.52 4.7e-07
2026-10-14 21:17:32 ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
COSMOS 2251 DEB
NORAD 36047
3.811 9.07 2.5e-07
2026-10-15 00:04:03 STARLINK-5137
NORAD 53975
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
4.738 12.75 3.6e-06
2026-10-15 16:37:15 SJ-12
NORAD 36596
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
3.209 14.92 1.6e-07
2026-10-15 19:27:08 ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
PLATFORM-6
NORAD 100611
4.473 14.12 1.1e-07
2026-10-15 20:18:40 ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
SL-14 DEB
NORAD 69735
4.448 10.01 1.7e-07
2026-10-15 20:43:14 GLOBAL-2
NORAD 43812
ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
2.906 14.93 2.0e-07
2026-10-17 13:03:49 ROBUSTA-3A (MEDITERRANEE)
NORAD 60243
FENGYUN 1C DEB
NORAD 30694
0.921 15.03 1.9e-06

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