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

ICEYE-X67

In orbit NORAD 66302 UZYQ-6182-0973-3502-7890

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-X67
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
534.30 km
Apogee
544.04 km
Inclination
45.4°
Period
95.4 min
Semi-major axis
6917.3 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 66302U 25248K   26283.62830808  .00001841  00000-0  12849-3 0  9995
2 66302  45.4057 244.7503 0006997 305.2126  54.8100 15.09531543 52965
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 12:03:27 STARLINK-4504
NORAD 53555 		ICEYE-X67
NORAD 66302 		3.255 6.30 1.2e-05
2026-10-12 11:17:50 MONOLITH
NORAD 49052 		ICEYE-X67
NORAD 66302 		3.141 3.96 4.3e-07
2026-10-13 13:07:57 LEMUR-2-THERMORAPTOR
NORAD 63354 		ICEYE-X67
NORAD 66302 		3.855 7.59 2.6e-07
2026-10-14 13:09:43 ICEYE-X67
NORAD 66302 		PSLV DEB
NORAD 27089 		2.008 11.33 7.8e-07
2026-10-15 00:07:07 ICEYE-X67
NORAD 66302 		ORIGAMISAT-2
NORAD 68795 		4.794 13.93 9.7e-08
2026-10-15 21:54:32 ICEYE-X67
NORAD 66302 		OBJECT A
NORAD 69538 		2.107 13.81 5.1e-07
2026-10-15 23:29:57 ICEYE-X67
NORAD 66302 		OBJECT A
NORAD 69538 		1.415 13.83 1.1e-06
2026-10-16 00:03:43 OBJECT E
NORAD 62733 		ICEYE-X67
NORAD 66302 		2.572 12.81 4.0e-07
2026-10-16 01:05:23 ICEYE-X67
NORAD 66302 		OBJECT A
NORAD 69538 		3.587 13.84 1.8e-07
2026-10-16 12:09:57 ICEYE-X67
NORAD 66302 		COSMOS 2251 DEB
NORAD 47116 		0.606 11.21 8.6e-06
2026-10-16 23:21:17 ICEYE-X67
NORAD 66302 		OBJECT A
NORAD 69538 		3.893 14.01 1.4e-07
2026-10-17 00:56:42 ICEYE-X67
NORAD 66302 		OBJECT A
NORAD 69538 		1.730 14.02 7.3e-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