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ICEYE-X71

In orbit NORAD 68494 HDKC-7956-9419-7008-7580

Observations 0
Satellite appearance

—

Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X71
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)
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
588.41 km
Apogee
590.41 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6967.5 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-07-10 21:59:08 UTC
Two-line elements (TLE)
1 68494U 26067CG  26191.33771511  .00001301  00000+0  13462-3 0  9992
2 68494  97.7615 149.2186 0001435   2.8077 357.3150 14.91779046 15172
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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 15:16:58 ICEYE-X71
NORAD 68494 		COSMOS 2251 DEB
NORAD 37975 		2.100 15.07 3.5e-07
2026-10-15 22:41:17 ICEYE-X71
NORAD 68494 		DELFI-N3XT
NORAD 39428 		1.600 4.74 1.6e-06
2026-10-15 23:14:09 QPS-SAR-14 (YACHIHOKO-I)
NORAD 66316 		ICEYE-X71
NORAD 68494 		3.330 9.30 3.2e-07
2026-10-16 08:20:33 ICEYE-X71
NORAD 68494 		COSMOS 921
NORAD 10095 		4.109 10.30 2.0e-07
2026-10-16 14:00:33 STARLINK-34644
NORAD 64812 		ICEYE-X71
NORAD 68494 		4.718 7.25 5.4e-06
2026-10-17 08:57:16 STARLINK-3086
NORAD 49178 		ICEYE-X71
NORAD 68494 		4.753 14.63 2.4e-06
2026-10-17 09:45:17 STARLINK-3086
NORAD 49178 		ICEYE-X71
NORAD 68494 		1.690 14.65 1.9e-05
2026-10-18 05:48:32 ICEYE-X71
NORAD 68494 		CZ-6A DEB
NORAD 54579 		3.831 13.16 1.7e-07
2026-10-18 06:51:30 STARLINK-3043
NORAD 49179 		ICEYE-X71
NORAD 68494 		4.730 14.95 2.2e-06
2026-10-18 18:53:18 ICEYE-X71
NORAD 68494 		ISIS 1 DEB
NORAD 36301 		3.334 15.55 1.4e-07
2026-10-19 01:40:41 ICEYE-X71
NORAD 68494 		CZ-6A DEB
NORAD 54412 		1.857 14.86 4.9e-07
2026-10-19 06:34:20 ICEYE-X71
NORAD 68494 		CZ-6A DEB
NORAD 54340 		4.020 14.25 1.3e-07
2026-10-19 13:01:38 OBJECT E
NORAD 61898 		ICEYE-X71
NORAD 68494 		0.717 12.28 5.5e-06
2026-10-20 15:27:36 ICEYE-X71
NORAD 68494 		FENGYUN 1C DEB
NORAD 36695 		1.914 2.61 1.2e-06

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