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ICEYE-X74

In orbit NORAD 68500 RBDW-0465-2136-9023-8478

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X74
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
586.26 km
Apogee
589.82 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6966.2 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 68500U 26067CN  26286.83769887  .00002769  00000-0  27713-3 0  9997
2 68500 97.7773 243.3915 0002561 28.4186 331.7172 14.92218321 29414
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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
2026-10-15 12:40:44 AAC-AIS-SAT1
NORAD 55107
ICEYE-X74
NORAD 68500
2.477 13.04 4.2e-07
2026-10-17 04:30:13 WNISAT-1
NORAD 39423
ICEYE-X74
NORAD 68500
4.586 15.04 7.5e-08
2026-10-17 21:46:51 ICEYE-X74
NORAD 68500
FENGYUN 1C DEB
NORAD 31057
3.631 13.81 1.7e-07
2026-10-18 05:56:10 ICEYE-X74
NORAD 68500
ICEYE-X77
NORAD 69892
3.770 7.22 2.8e-07
2026-10-18 21:51:47 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
4.855 14.64 7.6e-08
2026-10-18 23:28:21 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
3.410 14.64 1.5e-07
2026-10-18 23:43:06 ICEYE-X74
NORAD 68500
CZ-2D DEB
NORAD 43490
3.494 14.12 1.7e-07
2026-10-19 01:04:55 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
1.988 14.64 4.5e-07
2026-10-19 02:41:29 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
0.751 14.64 3.2e-06
2026-10-19 04:18:03 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
1.212 14.64 1.2e-06
2026-10-19 05:54:36 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
2.585 14.64 2.7e-07
2026-10-19 06:42:53 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
4.314 14.67 9.6e-08
2026-10-19 07:31:10 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
4.026 14.64 1.1e-07
2026-10-19 07:36:40 FFLY03
NORAD 65319
ICEYE-X74
NORAD 68500
1.527 12.71 1.2e-06
2026-10-19 08:19:27 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
3.053 14.67 1.9e-07
2026-10-19 09:56:01 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
2.094 14.67 4.1e-07
2026-10-19 11:32:35 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
1.956 14.67 4.7e-07
2026-10-19 13:09:08 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
2.765 14.67 2.3e-07
2026-10-19 14:45:42 IRIDE-MS2-HEO-4
NORAD 64582
ICEYE-X74
NORAD 68500
3.983 14.67 1.1e-07
2026-10-20 06:59:47 ICEYE-X74
NORAD 68500
SL-14 R/B
NORAD 11672
4.741 14.80 1.8e-07
2026-10-20 10:49:21 ICEYE-X74
NORAD 68500
COSMOS 2251 DEB
NORAD 36557
2.328 4.38 7.8e-07
2026-10-20 13:23:31 ICEYE-X74
NORAD 68500
DELTA 1 DEB
NORAD 26828
3.332 11.10 2.9e-07
2026-10-20 14:53:59 GRUS-3ALPHA
NORAD 64579
ICEYE-X74
NORAD 68500
1.281 14.68 1.1e-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