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

ICEYE-X80

In orbit NORAD 69893 QQKP-6798-9388-3562-2552

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X80
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
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
586.49 km
Apogee
593.42 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6968.1 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:57:00 UTC
Two-line elements (TLE)
1 69893U 26156AA  26283.53835522  .00002876  00000-0  29204-3 0  9992
2 69893 97.7443 182.3531 0005145 170.1085 190.0236 14.91608519 14191
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 20:31:48 ICEYE-X80
NORAD 69893
CZ-6A DEB
NORAD 56283
2.016 14.78 4.2e-07
2026-10-12 09:01:59 ICEYE-X80
NORAD 69893
CZ-6A DEB
NORAD 55532
3.586 14.89 1.3e-07
2026-10-14 16:42:51 ICEYE-X80
NORAD 69893
CZ-6A DEB
NORAD 56586
3.026 14.97 1.7e-07
2026-10-16 04:40:01 ICEYE-X52
NORAD 64572
ICEYE-X80
NORAD 69893
4.610 14.33 9.4e-08

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