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ERMIS-2

In orbit NORAD 68420 EALZ-0780-6325-0069-2307 Greece

Time in UTC

11.10 11:58

Scheduled · Сампо-400 [R1NAV]

113

Observations over 30 days

82%

Successful observations

111k

Frames, latest 2026-10-11 10:32 UTC

Mission information
Spacecraft name
ERMIS-2
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-03-30 13:20:00
Separation time
Last observers
Observer
Time of receipt
2026-10-11 10:32:48 UTC
2026-10-11 02:50:09 UTC
2026-10-11 01:18:18 UTC
2026-10-10 12:27:30 UTC
2026-10-05 12:28:33 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
496.74 km
Apogee
499.39 km
Inclination
97.5°
Period
94.6 min
Semi-major axis
6876.2 km
Velocity
7.62 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 68420U 26067E   26283.63612299  .00009901  00000-0  44192-3 0  9992
2 68420 97.4608 240.8907 0001923 117.3346 242.8085 15.21571993 29492
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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
2026-10-12 10:01:27 OBJECT B
NORAD 67747
ERMIS-2
NORAD 68420
3.459 15.05 1.3e-07
2026-10-12 11:36:11 OBJECT B
NORAD 67747
ERMIS-2
NORAD 68420
4.321 15.05 8.6e-08
2026-10-13 04:22:30 LEO EXPRESS 2
NORAD 62673
ERMIS-2
NORAD 68420
4.183 12.70 1.6e-07
2026-10-13 12:20:09 ERMIS-2
NORAD 68420
DRISHTI
NORAD 69010
1.222 7.71 2.6e-06
2026-10-13 13:07:29 ERMIS-2
NORAD 68420
DRISHTI
NORAD 69010
3.684 7.73 2.9e-07
2026-10-13 15:25:19 ALSAT-3B
NORAD 67646
ERMIS-2
NORAD 68420
4.479 12.75 1.3e-07
2026-10-14 04:50:16 OBJECT AD
NORAD 67275
ERMIS-2
NORAD 68420
4.397 12.76 1.4e-07
2026-10-14 08:49:20 HAWK-13A
NORAD 67392
ERMIS-2
NORAD 68420
1.905 5.16 1.2e-06
2026-10-14 19:12:46 ERMIS-2
NORAD 68420
COSMOS 374 DEB
NORAD 14122
1.726 10.79 1.1e-06
2026-10-14 20:04:19 STARLINK-5592
NORAD 55741
ERMIS-2
NORAD 68420
0.252 15.00 7.7e-04
2026-10-14 21:27:06 ERMIS-2
NORAD 68420
SL-14 R/B
NORAD 33505
4.520 14.97 8.0e-08
2026-10-15 13:58:53 OBJECT AK
NORAD 67281
ERMIS-2
NORAD 68420
2.564 12.75 4.1e-07
2026-10-15 22:05:05 STARLINK-5072
NORAD 55758
ERMIS-2
NORAD 68420
3.606 14.95 3.9e-06
2026-10-15 22:52:26 STARLINK-5072
NORAD 55758
ERMIS-2
NORAD 68420
4.074 14.93 3.0e-06
2026-10-16 03:23:48 FLOCK 4H-26
NORAD 66729
ERMIS-2
NORAD 68420
1.756 12.65 8.9e-07
2026-10-16 16:38:39 STARLINK-5677
NORAD 55463
ERMIS-2
NORAD 68420
3.057 10.04 1.1e-05
2026-10-16 22:01:30 ERMIS-2
NORAD 68420
STP-S29A OBJECT E
NORAD 68631
1.681 14.92 6.0e-07
2026-10-17 01:31:45 TOMORROW-S11
NORAD 67399
ERMIS-2
NORAD 68420
4.436 5.24 2.1e-07
2026-10-17 14:46:24 STARLINK-5918
NORAD 55939
ERMIS-2
NORAD 68420
2.795 15.01 6.3e-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