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ICEYE-X60

In orbit NORAD 66753 GASQ-1080-8348-1652-2247 Greece

Observations 0
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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-X60
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
531.52 km
Apogee
534.37 km
Inclination
97.4°
Period
95.4 min
Semi-major axis
6911.1 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 66753U 25276CR  26287.15744262  .00003585  00000-0  22398-3 0  9993
2 66753  97.4081 356.1202 0002065  19.3551 340.7757 15.10076205 48321
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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 15:58:01 ICEYE-X60
NORAD 66753 		RAAF M1
NORAD 43779 		4.471 3.88 2.1e-07
2026-10-16 20:35:49 ICEYE-X60
NORAD 66753 		CZ-2C DEB
NORAD 36090 		4.444 4.33 2.2e-07
2026-10-16 20:44:55 ICEYE-X60
NORAD 66753 		FENGYUN 1C DEB
NORAD 31536 		1.723 14.87 5.8e-07
2026-10-16 22:57:47 OBJECT A
NORAD 59810 		ICEYE-X60
NORAD 66753 		3.634 1.07 3.3e-07
2026-10-16 23:45:30 OBJECT A
NORAD 59810 		ICEYE-X60
NORAD 66753 		0.157 1.06 1.8e-04
2026-10-17 10:01:00 STARLINK-35043
NORAD 65436 		ICEYE-X60
NORAD 66753 		1.747 14.14 2.1e-05
2026-10-17 10:48:43 STARLINK-35043
NORAD 65436 		ICEYE-X60
NORAD 66753 		4.620 14.11 3.0e-06
2026-10-17 12:24:07 STARLINK-35043
NORAD 65436 		ICEYE-X60
NORAD 66753 		2.280 14.11 1.2e-05
2026-10-17 21:30:32 ICEYE-X60
NORAD 66753 		DISKSAT B
NORAD 67220 		4.943 14.07 8.8e-08
2026-10-18 03:13:34 ICEYE-X60
NORAD 66753 		DELTA 1 DEB
NORAD 8314 		3.388 15.07 1.4e-07
2026-10-18 12:03:34 CHUANGXIN 16A (CX-16A)
NORAD 53586 		ICEYE-X60
NORAD 66753 		4.049 12.54 1.7e-07
2026-10-20 08:05:34 ICEYE-X60
NORAD 66753 		CZ-4B DEB
NORAD 29042 		3.868 7.20 2.6e-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