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ICEYE-X52

In orbit NORAD 64572 ATHN-6625-5600-2788-0227 Finland

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X52
Other names
2025-135AW
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
2025-06-23 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
581.98 km
Apogee
583.38 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6960.8 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:58 UTC
Two-line elements (TLE)
1 64572U 25135AW  26283.62294218  .00001492  00000-0  14550-3 0  9999
2 64572 97.7849 36.6919 0000980 351.5623 8.5580 14.93941874 71112
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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 02:29:53 ICEYE-X52
NORAD 64572
ET-001B
NORAD 69941
4.554 14.34 9.6e-08
2026-10-11 10:32:09 ICEYE-X52
NORAD 64572
ET-001A
NORAD 69925
1.872 14.34 5.7e-07
2026-10-11 18:23:48 ICEYE-X52
NORAD 64572
CZ-2C DEB
NORAD 40289
2.636 14.97 2.3e-07
2026-10-11 20:59:37 ICEYE-X52
NORAD 64572
FOREST-19 (PATADASTRA)
NORAD 69001
3.253 14.17 1.9e-07
2026-10-13 05:56:16 ICEYE-X52
NORAD 64572
LEMUR-2-ALYX
NORAD 69928
4.141 14.34 1.2e-07
2026-10-13 11:00:51 ICEYE-X52
NORAD 64572
LEMUR-2-DELOITTE-3
NORAD 68471
3.214 14.69 1.7e-07
2026-10-13 17:24:27 ICEYE-X52
NORAD 64572
ELECTRON KICK STAGE R/B
NORAD 53354
4.975 14.51 7.6e-08
2026-10-13 18:12:42 ICEYE-X52
NORAD 64572
ELECTRON KICK STAGE R/B
NORAD 53354
2.696 14.49 2.6e-07
2026-10-14 16:28:41 ICEYE-X52
NORAD 64572
COSMOS 2251 DEB
NORAD 36557
4.489 14.92 8.0e-08
2026-10-15 03:12:03 ICEYE-X52
NORAD 64572
LEMUR-2-DELOITTE-2
NORAD 68491
2.120 14.69 4.0e-07
2026-10-16 04:40:01 ICEYE-X52
NORAD 64572
ICEYE-X80
NORAD 69893
4.610 14.33 9.4e-08
2026-10-16 12:49:31 KORSAT-7
NORAD 58463
ICEYE-X52
NORAD 64572
4.302 6.43 2.2e-07
2026-10-16 23:57:23 ICEYE-X52
NORAD 64572
TRANSPORTER-17 OBJECT J
NORAD 69877
4.200 14.33 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