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ICEYE-X59

In orbit NORAD 66752 TDJE-7079-9465-1938-8881 Greece

Observations 0
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2025

Falcon 9 Block 5 | Transporter 15 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X59
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 15 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2025-11-28 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
559.95 km
Apogee
561.11 km
Inclination
97.5°
Period
95.9 min
Semi-major axis
6938.7 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 66752U 25276CQ  26287.13892919  .00004191  00000-0  33195-3 0  9994
2 66752  97.4569 353.4962 0000841 100.7350 259.3969 15.01089333 48119
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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 12:40:02 ICEYE-X59
NORAD 66752 		COSMOS 397 DEB
NORAD 5144 		2.539 8.34 5.9e-07
2026-10-17 01:23:46 ICEYE-X59
NORAD 66752 		CZ-6A DEB
NORAD 61455 		4.173 3.26 2.5e-07
2026-10-17 03:36:56 ICEYE-X59
NORAD 66752 		COSMOS 2251 DEB
NORAD 35023 		3.136 7.15 4.0e-07
2026-10-17 09:14:15 STARLINK-5846
NORAD 56492 		ICEYE-X59
NORAD 66752 		4.834 11.03 4.2e-06
2026-10-17 10:59:20 ICEYE-X59
NORAD 66752 		COSMOS 2251 DEB
NORAD 37126 		4.695 12.71 1.2e-07
2026-10-17 13:05:30 ICEYE-X59
NORAD 66752 		STARLINK-36221
NORAD 67215 		4.534 4.52 6.2e-06
2026-10-17 21:26:03 ICEYE-X59
NORAD 66752 		COSMOS 2251 DEB
NORAD 37496 		1.316 7.19 2.3e-06
2026-10-18 11:04:01 ICEYE-X59
NORAD 66752 		OBJECT E
NORAD 65789 		2.004 13.40 6.1e-07
2026-10-19 02:20:21 ICEYE-X59
NORAD 66752 		DELTA 1 DEB
NORAD 26036 		1.309 14.88 9.8e-07
2026-10-20 07:00:39 ICEYE-X59
NORAD 66752 		SL-16 DEB
NORAD 22392 		4.889 14.29 8.5e-08
2026-10-20 11:56:51 ICEYE-X59
NORAD 66752 		COSMOS 2251 DEB
NORAD 36000 		4.740 15.08 6.8e-08
2026-10-20 15:41:30 HORACIO
NORAD 59098 		ICEYE-X59
NORAD 66752 		2.646 8.24 5.4e-07
2026-10-21 03:47:46 ICEYE-X59
NORAD 66752 		CINEMA-2 (KHUSAT-2)
NORAD 39424 		2.088 13.98 5.0e-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