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MICE-1

In orbit NORAD 66684 RGHP-8697-5632-9467-2081 Greece

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

22

Observations all time

Mission information
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 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-11-28 18:44:30
Separation time
2025-11-28 19:41:24
Last observers
Observer
Time of receipt
2026-05-13 20:54:15 UTC
2026-01-19 19:11:29 UTC
2026-01-14 15:47:45 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
500.36 km
Apogee
506.15 km
Inclination
97.4°
Period
94.7 min
Semi-major axis
6881.4 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 66684U 25276U   26282.43159440  .00002794  00000-0  13348-3 0  9996
2 66684 97.4179 354.1440 0004212 329.4416 30.6573 15.19852075 47769
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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 04:37:52 MICE-1
NORAD 66684
OBJECT B
NORAD 67249
4.205 1.93 2.5e-07
2026-10-11 05:25:41 MICE-1
NORAD 66684
RASSVET-3 22
NORAD 100088
0.328 14.51 1.8e-05
2026-10-11 07:12:56 S-NET B
NORAD 43187
MICE-1
NORAD 66684
2.729 15.00 2.2e-07
2026-10-11 23:46:37 SPACEMOBILE-003
NORAD 61045
MICE-1
NORAD 66684
3.117 13.79 2.4e-07
2026-10-12 01:21:22 SPACEMOBILE-003
NORAD 61045
MICE-1
NORAD 66684
4.170 13.77 1.3e-07
2026-10-12 11:11:24 TOMORROW-S9
NORAD 66309
MICE-1
NORAD 66684
4.644 13.90 1.0e-07
2026-10-12 12:16:40 MICE-1
NORAD 66684
HADES-SA (SPINNYONE)
NORAD 68446
3.784 12.69 1.9e-07
2026-10-13 05:36:21 BRO-20
NORAD 66674
MICE-1
NORAD 66684
3.429 0.12 3.8e-07
2026-10-13 06:58:44 HXMT (HUIYAN)
NORAD 42758
MICE-1
NORAD 66684
3.861 12.53 1.9e-07
2026-10-14 02:28:46 MICE-1
NORAD 66684
GEN1A-2
NORAD 69005
2.214 15.08 3.2e-07
2026-10-14 02:57:13 MICE-1
NORAD 66684
RASSVET-3 32
NORAD 100098
2.411 14.24 3.6e-07
2026-10-14 04:03:32 MICE-1
NORAD 66684
GEN1A-2
NORAD 69005
4.092 15.08 9.4e-08
2026-10-14 18:00:01 MICE-1
NORAD 66684
EMISAR
NORAD 68427
3.432 12.66 2.3e-07
2026-10-14 23:29:15 SDGSAT 1
NORAD 49387
MICE-1
NORAD 66684
1.211 3.82 2.9e-06
2026-10-15 02:39:55 MICE-1
NORAD 66684
CONNECTA IOT-15
NORAD 67402
2.689 9.12 5.0e-07
2026-10-15 05:01:05 SDGSAT 1
NORAD 49387
MICE-1
NORAD 66684
1.498 3.81 1.9e-06
2026-10-15 05:51:05 MICE-1
NORAD 66684
LUNA-2
NORAD 68470
3.093 12.74 2.8e-07
2026-10-15 14:50:48 CHAMRAN-1
NORAD 61072
MICE-1
NORAD 66684
3.360 4.43 3.8e-07
2026-10-15 19:13:20 MICE-1
NORAD 66684
FLOCK 4H-31
NORAD 66734
1.432 0.04 2.2e-06
2026-10-15 20:51:43 MICE-1
NORAD 66684
MARS-1
NORAD 68830
4.502 12.67 1.3e-07
2026-10-15 22:56:21 STARLINK-1522
NORAD 46027
MICE-1
NORAD 66684
3.552 14.41 4.8e-06
2026-10-16 07:22:06 MICE-1
NORAD 66684
USA 23
NORAD 18009
3.473 5.01 3.5e-07
2026-10-16 10:36:33 MICE-1
NORAD 66684
DELTA 1 DEB
NORAD 10184
3.294 8.78 3.4e-07
2026-10-16 22:31:25 TOMORROW-S9
NORAD 66309
MICE-1
NORAD 66684
4.304 14.41 1.1e-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