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ICEYE-X62

In orbit NORAD 66755 VNTG-7550-5151-2436-0152 Finland

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X62
Other names
2025-276CT
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
2025-11-28 00:00:00
Separation time
2025-11-28 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
530.40 km
Apogee
532.77 km
Inclination
97.4°
Period
95.3 min
Semi-major axis
6909.7 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 66755U 25276CT  26286.79037113  .00002153  00000-0  13440-3 0  9992
2 66755 97.4087 355.2488 0001715 357.6563 2.4658 15.10520868 48238
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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
2026-10-15 08:57:26 ICEYE-X62
NORAD 66755
PRSC-E03
NORAD 68835
4.034 11.99 1.8e-07
2026-10-16 03:46:51 OBJECT A
NORAD 63291
ICEYE-X62
NORAD 66755
1.576 8.85 1.5e-06
2026-10-16 18:06:49 OBJECT A
NORAD 61894
ICEYE-X62
NORAD 66755
4.864 0.24 1.9e-07
2026-10-16 22:52:30 ICEYE-X62
NORAD 66755
OBJECT D
NORAD 100783
1.659 0.62 1.6e-06
2026-10-17 04:26:22 ICEYE-X62
NORAD 66755
OBJECT D
NORAD 100783
2.544 0.63 6.8e-07
2026-10-17 06:29:59 ICEYE-X62
NORAD 66755
ZHUQUE-2E R/B
NORAD 69095
1.288 15.06 9.0e-07
2026-10-17 09:33:08 ICEYE-X62
NORAD 66755
KUIPER-00428
NORAD 69593
4.963 14.61 7.6e-08
2026-10-18 01:19:48 STARLINK-4513
NORAD 53548
ICEYE-X62
NORAD 66755
1.278 14.14 3.9e-05
2026-10-18 04:31:35 STARLINK-5171
NORAD 54077
ICEYE-X62
NORAD 66755
1.038 7.40 1.1e-04
2026-10-18 09:25:00 ICEYE-X62
NORAD 66755
FENGYUN 1C DEB
NORAD 38513
3.491 15.10 1.3e-07
2026-10-19 06:29:45 ICEYE-X62
NORAD 66755
OBJECT M
NORAD 42836
4.843 10.61 1.4e-07
2026-10-19 07:17:26 ICEYE-X62
NORAD 66755
OBJECT M
NORAD 42836
1.361 10.64 1.8e-06
2026-10-20 07:10:55 NANOFF B
NORAD 58755
ICEYE-X62
NORAD 66755
4.361 0.34 2.3e-07
2026-10-20 15:06:45 ICEYE-X62
NORAD 66755
OBJECT D
NORAD 68201
2.080 0.63 1.0e-06
2026-10-20 21:49:37 STARLINK-5189
NORAD 54052
ICEYE-X62
NORAD 66755
1.418 5.84 6.2e-05

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