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ERMIS-1

In orbit NORAD 68468 DJQS-0588-0767-3427-2831 Greece

Time in UTC

16.10 10:44

Scheduled · Сампо-400 [R1NAV]

255

Observations over 30 days

75%

Successful observations

124k

Frames, latest 2026-10-14 11:17 UTC

Mission information
Spacecraft name
ERMIS-1
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
2026-10-14 11:17:03 UTC
2026-10-13 13:12:53 UTC
2026-10-13 10:04:42 UTC
2026-10-13 03:56:41 UTC
2026-10-13 02:24:42 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
499.80 km
Apogee
509.79 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6882.9 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68468U 26067BE  26287.12991012  .00008562  00000-0  40796-3 0  9993
2 68468 97.4699 243.9148 0007262 21.1391 339.0142 15.19342942 29983
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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
2026-10-15 22:46:13 ERMIS-1
NORAD 68468
CZ-4B DEB
NORAD 43430
3.249 10.76 3.1e-07
2026-10-15 22:46:14 STARLINK-3107
NORAD 49171
ERMIS-1
NORAD 68468
4.888 15.02 2.0e-06
2026-10-16 10:00:15 ERMIS-1
NORAD 68468
CZ-4B R/B
NORAD 44531
3.891 10.91 2.1e-07
2026-10-18 02:56:56 STARLINK-5921
NORAD 55926
ERMIS-1
NORAD 68468
3.866 14.99 3.3e-06
2026-10-18 19:41:04 FLOCK 4H-24
NORAD 66727
ERMIS-1
NORAD 68468
2.576 12.73 4.1e-07
2026-10-19 01:15:09 SUPERVIEW NEO-2 06
NORAD 68378
ERMIS-1
NORAD 68468
1.264 6.22 2.5e-06
2026-10-19 01:15:09 SUPERVIEW NEO-2 05
NORAD 68377
ERMIS-1
NORAD 68468
0.516 6.22 1.5e-05
2026-10-19 02:49:06 SHIJIAN-6 03A (SJ-6 03A)
NORAD 33408
ERMIS-1
NORAD 68468
3.520 9.77 2.8e-07
2026-10-19 03:37:22 SUPERVIEW NEO-2 05
NORAD 68377
ERMIS-1
NORAD 68468
1.899 6.24 1.1e-06
2026-10-19 03:37:22 SUPERVIEW NEO-2 06
NORAD 68378
ERMIS-1
NORAD 68468
2.087 6.24 9.4e-07
2026-10-19 07:19:45 OBJECT E
NORAD 67750
ERMIS-1
NORAD 68468
2.957 15.02 1.8e-07
2026-10-19 09:48:49 CONNECTA IOT-11
NORAD 64557
ERMIS-1
NORAD 68468
3.558 14.81 1.4e-07
2026-10-19 12:21:20 AISSAT 4
NORAD 68454
ERMIS-1
NORAD 68468
4.375 0.01 2.3e-07
2026-10-19 19:23:34 JILIN-1 GAOFEN 2B
NORAD 44836
ERMIS-1
NORAD 68468
0.297 12.69 3.1e-05
2026-10-20 03:33:44 STARLINK-3121
NORAD 49428
ERMIS-1
NORAD 68468
1.529 7.78 5.0e-05

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