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ICEYE-X81

In orbit NORAD 69889 YBOB-6098-6823-8093-3505

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X81
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
585.87 km
Apogee
592.93 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6967.5 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 69889U 26156W   26283.80520034  .00003826  00000-0  38494-3 0  9993
2 69889 97.7449 182.6271 0005070 170.4669 189.6647 14.91780640 14235
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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 14:03:09 ICEYE-X81
NORAD 69889
CZ-6A DEB
NORAD 56283
1.804 14.78 5.3e-07
2026-10-11 14:11:53 ICEYE-X81
NORAD 69889
FENGYUN 1C DEB
NORAD 31878
3.427 10.40 2.9e-07
2026-10-12 04:01:43 GRUS-3ALPHA
NORAD 64579
ICEYE-X81
NORAD 69889
4.432 14.33 1.0e-07
2026-10-12 16:47:59 ICEYE-X81
NORAD 69889
LEMUR-2-SOPHILUNA-X1
NORAD 69930
3.840 0.02 3.0e-07
2026-10-12 21:09:32 ICEYE-X81
NORAD 69889
OBJECT J
NORAD 44887
3.711 14.96 1.1e-07
2026-10-12 22:30:11 ICEYE-X81
NORAD 69889
COSMOS 2251 DEB
NORAD 34854
3.163 11.42 3.1e-07
2026-10-12 22:46:05 ICEYE-X81
NORAD 69889
OBJECT J
NORAD 44887
2.415 14.96 2.7e-07
2026-10-13 00:22:39 ICEYE-X81
NORAD 69889
OBJECT J
NORAD 44887
4.043 14.96 9.7e-08
2026-10-13 08:01:52 ICEYE-X81
NORAD 69889
CZ-4B DEB
NORAD 40530
4.296 14.24 1.1e-07
2026-10-14 01:45:16 ICEYE-X81
NORAD 69889
RUBIN-8 & PSLV R/B
NORAD 32792
2.946 11.94 3.4e-07
2026-10-14 03:47:25 ICEYE-X81
NORAD 69889
CZ-6A DEB
NORAD 56586
4.627 14.97 7.4e-08
2026-10-15 10:25:14 ICEYE-X81
NORAD 69889
UNISAT-2
NORAD 27608
3.509 14.95 1.3e-07
2026-10-16 03:37:30 XINZHENGCHENG-01
NORAD 68412
ICEYE-X81
NORAD 69889
2.506 5.05 6.7e-07
2026-10-16 08:22:53 ICEYE-X81
NORAD 69889
SL-16 DEB
NORAD 22338
1.425 6.28 2.0e-06
2026-10-16 16:04:45 ICEYE-X81
NORAD 69889
FENGYUN 1C DEB
NORAD 31837
3.574 14.98 1.2e-07
2026-10-16 16:36:32 ICEYE-X81
NORAD 69889
FENGYUN 1C DEB
NORAD 32409
4.785 3.96 1.9e-07
2026-10-17 07:05:32 IRIS
NORAD 39197
ICEYE-X81
NORAD 69889
4.492 7.46 1.9e-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