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ICEYE-X62

In orbit NORAD 66755 VNTG-7550-5151-2436-0152 Finland

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-X62
Other names
2025-276CT
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
2025-11-28 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
530.29 km
Apogee
532.96 km
Inclination
97.4°
Period
95.3 min
Semi-major axis
6909.7 km
Velocity
7.58 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 13:08:42 UTC
Two-line elements (TLE)
1 66755U 25276CT  26285.20050660  .00002618  00000-0  16263-3 0  9991
2 66755  97.4092 353.7103 0001831   4.5336 355.5910 15.10514663 47997
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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
2026-10-13 16:11:03 ICEYE-X62
NORAD 66755 		FRAMSAT-1
NORAD 100610 		3.432 0.69 3.7e-07
2026-10-15 07:19:58 ICEYE-X62
NORAD 66755 		SL-12 DEB
NORAD 41677 		2.958 16.61 2.0e-07
2026-10-15 08:57:25 ICEYE-X62
NORAD 66755 		PRSC-E03
NORAD 68835 		4.032 11.99 1.8e-07
2026-10-16 03:46:50 OBJECT A
NORAD 63291 		ICEYE-X62
NORAD 66755 		3.076 8.85 3.9e-07
2026-10-16 18:06:49 OBJECT A
NORAD 61894 		ICEYE-X62
NORAD 66755 		3.777 0.24 3.1e-07
2026-10-16 21:17:05 ICEYE-X62
NORAD 66755 		OBJECT D
NORAD 100783 		1.896 0.62 1.2e-06
2026-10-17 02:50:57 ICEYE-X62
NORAD 66755 		OBJECT D
NORAD 100783 		1.769 0.63 1.4e-06
2026-10-17 06:30:01 ICEYE-X62
NORAD 66755 		ZHUQUE-2E R/B
NORAD 69095 		4.334 15.06 7.9e-08
2026-10-18 04:31:34 STARLINK-5171
NORAD 54077 		ICEYE-X62
NORAD 66755 		3.105 7.40 1.2e-05
2026-10-19 00:57:20 ICEYE-X62
NORAD 66755 		OBJECT A
NORAD 68198 		4.210 0.61 2.5e-07
2026-10-19 08:52:47 ICEYE-X62
NORAD 66755 		OBJECT M
NORAD 42836 		0.561 10.64 1.1e-05

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