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ICEYE-X33

In orbit NORAD 60548 GZXN-1336-4265-9976-3059 United States of America

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X33
Other names
2024-129CJ
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
2024-08-16 00:00:00
Separation time
2024-08-16 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
558.58 km
Apogee
561.15 km
Inclination
97.8°
Period
95.9 min
Semi-major axis
6938.0 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:44 UTC
Two-line elements (TLE)
1 60548U 24149CJ  26284.29652728  .00004814  00000-0  37871-3 0  9992
2 60548 97.7531 3.0218 0001877 68.9164 291.2260 15.01311091117629
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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 01:04:39 ICEYE-X33
NORAD 60548
CUBEBUG-1 (CAPITAN BETO)
NORAD 39153
3.514 10.30 2.7e-07
2026-10-12 14:26:11 ICEYE-X33
NORAD 60548
FENGYUN 1C DEB
NORAD 31898
0.940 14.99 1.8e-06
2026-10-13 17:41:32 ICEYE-X33
NORAD 60548
COSMOS 249 DEB
NORAD 19317
1.017 6.38 3.9e-06
2026-10-14 05:54:50 ICEYE-X33
NORAD 60548
PEGASUS DEB
NORAD 24007
2.837 14.09 2.6e-07
2026-10-14 08:56:20 ICEYE-X33
NORAD 60548
ATLAS 5 CENTAUR R/B
NORAD 31702
4.519 14.48 9.6e-08
2026-10-17 01:16:49 ICEYE-X33
NORAD 60548
SL-19 R/B
NORAD 36039
4.827 14.88 7.2e-08
2026-10-17 03:25:54 ICEYE-X33
NORAD 60548
SCOUT X-4 DEB
NORAD 3750
1.916 14.79 4.7e-07
2026-10-17 09:03:59 ICEYE-X33
NORAD 60548
ICEYE-X53
NORAD 64584
3.203 4.82 4.1e-07
2026-10-17 09:11:38 ICEYE-X33
NORAD 60548
CINEMA-2 (KHUSAT-2)
NORAD 39424
4.204 14.50 1.1e-07
2026-10-17 11:25:30 ICEYE-X33
NORAD 60548
CZ-4C DEB
NORAD 37567
4.335 12.56 1.5e-07
2026-10-17 12:54:38 GRUS-1B
NORAD 47934
ICEYE-X33
NORAD 60548
3.937 14.78 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