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ICEYE-X54

In orbit NORAD 64570 KKTB-3799-7177-0689-2786 Finland

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X54
Other names
2025-135AU
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
2025-06-23 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
578.47 km
Apogee
580.21 km
Inclination
97.8°
Period
96.3 min
Semi-major axis
6957.5 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 64570U 25135AU  26284.29924484  .00003092  00000-0  28793-3 0  9998
2 64570 97.7828 37.6913 0001279 307.5066 52.6038 14.95019376 71243
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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 12:45:09 ICEYE-X54
NORAD 64570
DELTA 1 DEB
NORAD 7850
3.668 14.78 1.3e-07
2026-10-13 16:27:43 AEROCUBE 5C
NORAD 40965
ICEYE-X54
NORAD 64570
2.369 14.35 3.5e-07
2026-10-14 16:32:12 ICEYE-X54
NORAD 64570
COSMOS 252 DEB
NORAD 3565
2.300 7.88 7.3e-07
2026-10-14 19:00:25 ICEYE-X54
NORAD 64570
LEMUR-2-NURAY
NORAD 69932
4.036 14.32 1.2e-07
2026-10-15 08:37:23 ICEYE-X54
NORAD 64570
COSMOS 2251 DEB
NORAD 36557
4.906 14.97 6.6e-08
2026-10-15 19:06:04 ICEYE-X54
NORAD 64570
ET-001B
NORAD 69941
4.925 14.32 8.2e-08
2026-10-16 04:16:09 APRIZESAT 8
NORAD 39425
ICEYE-X54
NORAD 64570
4.352 14.91 8.7e-08
2026-10-16 07:15:48 ICEYE-X54
NORAD 64570
TRISAT-S
NORAD 100612
3.937 5.09 2.7e-07
2026-10-16 12:04:57 ICEYE-X54
NORAD 64570
OBJECT A
NORAD 100609
3.595 5.09 3.2e-07
2026-10-17 04:57:16 ICEYE-X54
NORAD 64570
SKYCRAFT-4C
NORAD 64896
1.912 6.57 1.1e-06
2026-10-17 11:42:10 ICEYE-X54
NORAD 64570
CZ-6A DEB
NORAD 60672
4.331 15.13 8.0e-08

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