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ICEYE-X50

In orbit NORAD 63255 IZVD-0255-5665-7405-4547 Finland

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X50
Other names
2025-052AX
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
2025-03-15 00:00:00
Separation time
2025-05-15 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
576.00 km
Apogee
579.18 km
Inclination
97.7°
Period
96.3 min
Semi-major axis
6955.7 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 63255U 25052AX  26283.58045444  .00002069  00000-0  19154-3 0  9990
2 63255 97.6713 173.1692 0002304 138.4679 221.6718 14.95579370 85899
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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
2026-10-10 23:17:44 ICEYE-X50
NORAD 63255
OBJECT P
NORAD 100968
4.302 14.57 9.9e-08
2026-10-11 00:54:05 ICEYE-X50
NORAD 63255
OBJECT N
NORAD 100967
4.987 14.57 7.4e-08
2026-10-11 02:35:15 ETRSS-1
NORAD 44880
ICEYE-X50
NORAD 63255
4.322 14.86 8.8e-08
2026-10-11 04:06:46 ICEYE-X50
NORAD 63255
OBJECT M
NORAD 100966
4.246 14.57 1.0e-07
2026-10-11 07:19:27 ICEYE-X50
NORAD 63255
OBJECT J
NORAD 100963
3.942 14.57 1.2e-07
2026-10-11 13:39:07 ICEYE-X50
NORAD 63255
CZ-4B DEB
NORAD 26273
3.875 10.40 2.2e-07
2026-10-11 18:30:55 ICEYE-X50
NORAD 63255
ARVAKER-2
NORAD 64567
3.816 13.91 1.5e-07
2026-10-12 07:24:34 ICEYE-X50
NORAD 63255
OBJECT G
NORAD 100961
2.240 14.57 3.7e-07
2026-10-12 15:26:18 ICEYE-X50
NORAD 63255
OBJECT F
NORAD 100960
0.763 14.57 3.2e-06
2026-10-12 18:38:59 ICEYE-X50
NORAD 63255
OBJECT E
NORAD 100959
0.418 14.57 1.0e-05
2026-10-13 02:40:41 ICEYE-X50
NORAD 63255
OBJECT B
NORAD 100956
1.978 14.57 4.7e-07
2026-10-13 07:29:44 ICEYE-X50
NORAD 63255
OBJECT A
NORAD 100955
1.100 14.57 1.5e-06
2026-10-14 02:11:59 TIMED
NORAD 26998
ICEYE-X50
NORAD 63255
3.179 15.10 1.5e-07
2026-10-14 02:41:44 ICEYE-X50
NORAD 63255
COSMOS 2251 DEB
NORAD 37487
4.101 13.10 1.5e-07
2026-10-14 05:55:33 ICEYE-X50
NORAD 63255
SATORO-T3
NORAD 64589
2.211 13.89 4.5e-07
2026-10-14 12:58:11 ICEYE-X50
NORAD 63255
CZ-2D R/B
NORAD 36597
2.823 14.23 2.6e-07
2026-10-16 04:45:05 ICEYE-X50
NORAD 63255
FFLY01
NORAD 65320
4.965 14.99 6.4e-08
2026-10-16 23:23:42 ICEYE-X50
NORAD 63255
SKYKRAFT-4D
NORAD 64898
3.321 14.96 1.4e-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