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

ICEYE-X61

In orbit NORAD 66754 CHSD-3041-8652-4646-6982

Satellite appearance

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X61
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
505.47 km
Apogee
508.52 km
Inclination
97.4°
Period
94.8 min
Semi-major axis
6885.1 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-07-17 13:58:52 UTC
Two-line elements (TLE)
1 66754U 25276CS  26197.74724750  .00001571  00000+0  79163-4 0  9994
2 66754 97.4193 270.6864 0002212 207.8838 152.2279 15.18614124 34906
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
2026-10-15 09:07:26 CENTAURI-1
NORAD 43809
ICEYE-X61
NORAD 66754
2.343 2.89 7.9e-07
2026-10-15 22:33:34 ICEYE-X61
NORAD 66754
TRANSPORTER-18 OBJECT AP
NORAD 100920
2.275 0.26 8.5e-07
2026-10-15 22:33:36 ICEYE-X61
NORAD 66754
RADIX-MK
NORAD 100940
2.989 0.26 4.9e-07
2026-10-16 18:21:54 ICEYE-X61
NORAD 66754
IRIDE-MS1-EAGLET 2-12
NORAD 68461
4.340 12.65 1.4e-07
2026-10-16 19:09:19 ICEYE-X61
NORAD 66754
IRIDE-MS1-EAGLET 2-12
NORAD 68461
4.298 12.68 1.5e-07
2026-10-16 19:56:45 ICEYE-X61
NORAD 66754
IRIDE-MS1-EAGLET 2-12
NORAD 68461
2.396 12.65 4.8e-07
2026-10-17 20:38:24 ICEYE-X61
NORAD 66754
STARLINK-37522
NORAD 69446
3.392 7.11 1.0e-05
2026-10-17 21:14:20 ICEYE-X61
NORAD 66754
DB-PFW
NORAD 68466
4.807 12.67 1.2e-07
2026-10-17 22:01:45 ICEYE-X61
NORAD 66754
DB-PFW
NORAD 68466
4.578 12.70 1.3e-07
2026-10-17 22:49:12 ICEYE-X61
NORAD 66754
DB-PFW
NORAD 68466
4.718 12.67 1.2e-07
2026-10-17 23:36:36 ICEYE-X61
NORAD 66754
DB-PFW
NORAD 68466
3.912 12.70 1.8e-07
2026-10-18 01:11:27 ICEYE-X61
NORAD 66754
DB-PFW
NORAD 68466
4.143 12.70 1.6e-07
2026-10-18 04:18:30 ICEYE-X61
NORAD 66754
TERRA NOVA
NORAD 100909
1.089 0.25 3.7e-06
2026-10-18 18:32:07 ICEYE-X61
NORAD 66754
HADES-L
NORAD 100938
2.981 0.25 5.0e-07
2026-10-19 08:00:58 ICEYE-X61
NORAD 66754
VEGAFLY-1
NORAD 68430
4.229 12.64 1.5e-07
2026-10-21 02:48:44 SPACEMOBILE-001
NORAD 61047
ICEYE-X61
NORAD 66754
2.664 10.78 4.6e-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