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ERMIS-3

In orbit NORAD 68425 ZRPV-6317-0836-0013-3209 Greece

Time in UTC

13:17

Next pass · ИТ-куб, Калининград · 35°

13.10 00:41

Scheduled · Сампо-400 [R1NAV]

89

Observations over 30 days

77%

Successful observations

61k

Frames, latest 2026-10-12 11:53 UTC

Mission information
Spacecraft name
ERMIS-3
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
2026-10-12 11:53:22 UTC
2026-10-12 10:18:52 UTC
2026-10-12 02:37:45 UTC
2026-10-12 01:04:24 UTC
2026-10-11 12:11:12 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
502.62 km
Apogee
503.65 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6881.2 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:37 UTC
Two-line elements (TLE)
1 68425U 26067K   26284.62583496  .00008283  00000-0  38873-3 0  9994
2 68425 97.4735 241.8448 0000712 46.2333 313.8961 15.19898848 29625
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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 23:44:59 ERMIS-3
NORAD 68425
YAOGAN-1 DEB
NORAD 36365
4.210 12.96 1.5e-07
2026-10-13 10:38:13 ERMIS-3
NORAD 68425
MISR-C-1
NORAD 68628
3.792 14.69 1.3e-07
2026-10-15 16:53:54 ERMIS-3
NORAD 68425
GSLV R/B
NORAD 56760
4.852 12.78 1.4e-07
2026-10-15 18:12:53 ERMIS-3
NORAD 68425
ELECTRON KICK STAGE R/B
NORAD 45728
4.875 12.33 1.2e-07
2026-10-17 04:47:04 CONNECTA IOT-10
NORAD 64555
ERMIS-3
NORAD 68425
4.867 14.76 7.5e-08
2026-10-17 10:51:51 BLACKJACK ACES-2
NORAD 56955
ERMIS-3
NORAD 68425
2.415 15.08 2.7e-07
2026-10-17 12:21:59 OBJECT F
NORAD 63296
ERMIS-3
NORAD 68425
2.831 15.08 2.0e-07
2026-10-17 12:26:41 BLACKJACK ACES-2
NORAD 56955
ERMIS-3
NORAD 68425
2.176 15.08 3.3e-07
2026-10-17 13:56:50 OBJECT F
NORAD 63296
ERMIS-3
NORAD 68425
4.043 15.08 9.6e-08
2026-10-17 14:01:30 BLACKJACK ACES-2
NORAD 56955
ERMIS-3
NORAD 68425
4.818 15.08 6.8e-08
2026-10-17 14:48:55 BLACKJACK ACES-2
NORAD 56955
ERMIS-3
NORAD 68425
3.690 15.09 1.2e-07
2026-10-17 16:23:44 BLACKJACK ACES-2
NORAD 56955
ERMIS-3
NORAD 68425
3.331 15.09 1.4e-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