RU | EN | ZH --:-- UTC Sign in
Back

ICEYE-X65

In orbit NORAD 66300 XXVL-0580-8820-0681-1988

Observations 0
Go to map
Back

—

Falcon 9 Block 5 | Bandwagon 4 (Dedicated Mid-Inclination Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 40

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X65
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 | Bandwagon 4 (Dedicated Mid-Inclination Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 40
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
538.89 km
Apogee
547.11 km
Inclination
45.4°
Period
95.5 min
Semi-major axis
6921.1 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:59 UTC
Two-line elements (TLE)
1 66300U 25248H   26283.61173587  .00001672  00000-0  12205-3 0  9994
2 66300  45.4052 247.0579 0005871 305.9399  54.0938 15.08279919 52940
Copy content
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 20:32:35 SEDNA-2
NORAD 63153 		ICEYE-X65
NORAD 66300 		4.981 12.65 1.1e-07
2026-10-12 08:25:05 ICEYE-X65
NORAD 66300 		OBJECT A
NORAD 60235 		2.478 5.92 6.7e-07
2026-10-13 08:47:22 ICEYE-X65
NORAD 66300 		KAKUSHIN RISING OBJECT B
NORAD 68793 		3.804 14.21 1.4e-07
2026-10-13 14:38:02 ICEYE-X65
NORAD 66300 		DELTA 1 DEB
NORAD 12227 		2.073 11.40 7.3e-07
2026-10-13 15:17:53 ICEYE-X65
NORAD 66300 		DELTA 2 R/B
NORAD 25876 		4.597 7.48 1.9e-07
2026-10-13 22:53:41 ICEYE-X65
NORAD 66300 		CZ-4C R/B
NORAD 43264 		1.676 6.84 1.4e-06
2026-10-15 08:41:37 SWAS
NORAD 25560 		ICEYE-X65
NORAD 66300 		2.563 6.60 6.1e-07
2026-10-15 09:09:11 ICEYE-X65
NORAD 66300 		NEONSAT-1A
NORAD 67614 		2.824 14.40 2.5e-07
2026-10-15 19:12:02 ICEYE-X65
NORAD 66300 		COSMOS 2251 DEB
NORAD 36000 		3.701 5.50 3.0e-07
2026-10-16 05:29:37 ICEYE-X65
NORAD 66300 		CZ-4B DEB
NORAD 38326 		3.194 13.20 2.5e-07
2026-10-16 12:29:42 ICEYE-X65
NORAD 66300 		OBJECT D
NORAD 100146 		3.588 10.51 2.6e-07
2026-10-16 12:32:57 ICEYE-X65
NORAD 66300 		CZ-4B DEB
NORAD 36290 		0.810 11.65 4.7e-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