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ICEYE-X63

In orbit NORAD 67372 FRPZ-5087-2399-8068-4647 Finland

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X63
Other names
2026-004K
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
2026-01-11 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
595.81 km
Apogee
603.69 km
Inclination
97.8°
Period
96.7 min
Semi-major axis
6977.9 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:45 UTC
Two-line elements (TLE)
1 67372U 26004K   26284.25176711  .00000813  00000-0  93429-4 0  9992
2 67372 97.8085 281.1386 0005672 102.2719 257.9133 14.88469239 40564
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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 16:21:56 ICEYE-X63
NORAD 67372
TRANSPORTER-17 OBJECT AU
NORAD 69911
4.805 11.33 1.4e-07
2026-10-12 20:28:43 ICEYE-X63
NORAD 67372
COSMOS 1174 DEB
NORAD 11778
3.287 14.21 2.0e-07
2026-10-13 04:21:11 ICEYE-X63
NORAD 67372
CZ-4B DEB
NORAD 26207
4.075 13.42 1.4e-07
2026-10-13 18:30:40 ICEYE-X63
NORAD 67372
FENGYUN 1C DEB
NORAD 31541
2.640 14.98 2.3e-07
2026-10-14 18:08:45 ICEYE-X63
NORAD 67372
ORBCOMM FM111
NORAD 40089
4.749 12.61 1.2e-07
2026-10-14 20:02:00 ICEYE-X63
NORAD 67372
DELTA 1 DEB
NORAD 7839
4.513 13.66 1.1e-07
2026-10-15 12:08:18 ICEYE-X63
NORAD 67372
SL-14 R/B
NORAD 12786
4.972 8.54 3.6e-07
2026-10-15 17:21:19 GEESAT-6 03
NORAD 65715
ICEYE-X63
NORAD 67372
4.402 14.51 9.7e-08
2026-10-16 09:50:17 ICEYE-X63
NORAD 67372
CZ-6A DEB
NORAD 54471
4.533 9.14 1.8e-07
2026-10-17 12:30:13 DX1
NORAD 40071
ICEYE-X63
NORAD 67372
2.178 3.56 9.1e-07
2026-10-17 13:16:36 ICEYE-X63
NORAD 67372
CZ-6A DEB
NORAD 55543
2.906 5.94 4.9e-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