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ICEYE-X79

In orbit NORAD 69870 ZCNX-3156-7544-6374-9036

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X79
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
584.49 km
Apogee
593.17 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6967.0 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:21 UTC
Two-line elements (TLE)
1 69870U 26156B   26282.44820324  .00001817  00000-0  18484-3 0  9992
2 69870 97.7418 181.2878 0006230 183.1200 176.9982 14.91964400 14037
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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 01:33:39 ICEYE-X79
NORAD 69870
OBJECT F
NORAD 100463
1.085 14.89 1.4e-06
2026-10-12 20:25:03 ICEYE-X79
NORAD 69870
GRUS-3B
NORAD 69918
3.522 0.01 3.6e-07
2026-10-12 21:15:37 ICEYE-X79
NORAD 69870
GRUS-3B
NORAD 69918
3.037 0.01 4.8e-07
2026-10-12 22:02:01 ICEYE-X79
NORAD 69870
GRUS-3B
NORAD 69918
0.251 0.01 7.0e-05
2026-10-12 22:50:07 ICEYE-X79
NORAD 69870
GRUS-3B
NORAD 69918
0.785 0.01 7.1e-06
2026-10-12 23:39:02 ICEYE-X79
NORAD 69870
GRUS-3B
NORAD 69918
3.031 0.01 4.8e-07
2026-10-13 00:24:49 ICEYE-X79
NORAD 69870
GRUS-3B
NORAD 69918
3.553 0.01 3.5e-07
2026-10-14 16:41:19 LEMUR-2-IRINA
NORAD 68480
ICEYE-X79
NORAD 69870
2.948 7.29 4.5e-07
2026-10-15 00:42:46 ICEYE-X79
NORAD 69870
CZ-2D DEB
NORAD 43487
4.131 11.80 1.8e-07
2026-10-15 01:38:12 BRITE-CA1 (TORONTO)
NORAD 40020
ICEYE-X79
NORAD 69870
4.136 13.68 1.3e-07
2026-10-15 07:12:23 ICEYE-X79
NORAD 69870
FENGYUN 1C DEB
NORAD 31269
3.007 3.49 4.8e-07
2026-10-15 16:51:46 ICEYE-X79
NORAD 69870
NAVIGATOR
NORAD 69887
3.176 0.01 4.1e-07
2026-10-15 17:39:01 ICEYE-X79
NORAD 69870
NAVIGATOR
NORAD 69887
1.733 0.01 1.4e-06
2026-10-16 12:11:01 ICEYE-X79
NORAD 69870
TOM-2
NORAD 69914
4.099 0.01 2.6e-07
2026-10-16 23:48:52 ICEYE-X79
NORAD 69870
CZ-6A DEB
NORAD 54579
2.964 14.97 1.8e-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