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ICEYE-X85

In orbit NORAD 100914 BFIE-6843-0330-0537-8587

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X85
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
507.20 km
Apogee
512.78 km
Inclination
97.4°
Period
94.9 min
Semi-major axis
6888.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:06 UTC
Two-line elements (TLE)
1 A0914U 26227AH  26287.27601792  .00006892  00000-0  34553-3 0  9990
2 A0914 97.4410 356.5774 0004070 103.3476 256.8212 15.17653771 1902
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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 08:23:08 IRIDE-MS1-EAGLET 2-12
NORAD 68461
ICEYE-X85
NORAD 100914
4.895 12.54 1.2e-07
2026-10-15 09:30:03 ICEYE-X85
NORAD 100914
ARIANE 5 DEB
NORAD 45247
4.005 12.89 2.0e-07
2026-10-15 13:21:24 YAOGAN-36 05C
NORAD 57456
ICEYE-X85
NORAD 100914
2.349 9.38 6.5e-07
2026-10-16 15:12:00 EAGLET-I
NORAD 43790
ICEYE-X85
NORAD 100914
4.871 2.98 1.8e-07
2026-10-16 22:26:36 ICEYE-X85
NORAD 100914
COSMOS 2251 DEB
NORAD 34856
3.905 15.01 1.1e-07
2026-10-17 04:41:31 IRIDE-MS1-EAGLET 2-16
NORAD 68452
ICEYE-X85
NORAD 100914
4.713 12.54 1.3e-07
2026-10-17 10:19:47 STP-S29A OBJECT E
NORAD 68631
ICEYE-X85
NORAD 100914
3.875 9.34 2.4e-07
2026-10-18 12:27:22 TRANSPORTER-18 OBJECT AF
NORAD 100912
ICEYE-X85
NORAD 100914
1.189 0.00 6.3e-06
2026-10-18 12:51:49 TRANSPORTER-18 OBJECT AF
NORAD 100912
ICEYE-X85
NORAD 100914
0.834 0.00 6.3e-06
2026-10-18 15:59:56 YAOGAN-39 03C
NORAD 57990
ICEYE-X85
NORAD 100914
1.662 12.43 1.0e-06
2026-10-19 15:59:17 SIRION PATHFINDER-2
NORAD 43759
ICEYE-X85
NORAD 100914
2.854 3.02 5.3e-07
2026-10-19 16:43:44 ICEYE-X85
NORAD 100914
TRANSPORTER-18 OBJECT AK
NORAD 100916
4.454 0.01 2.2e-07
2026-10-19 18:18:33 ICEYE-X85
NORAD 100914
TRANSPORTER-18 OBJECT AK
NORAD 100916
2.702 0.00 7.0e-05
2026-10-19 19:53:09 ICEYE-X85
NORAD 100914
TRANSPORTER-18 OBJECT AK
NORAD 100916
0.942 0.00 7.0e-05
2026-10-19 21:08:45 ICEYE-X85
NORAD 100914
TRANSPORTER-18 OBJECT AK
NORAD 100916
0.676 0.00 7.0e-05
2026-10-19 22:07:20 ICEYE-X85
NORAD 100914
TRANSPORTER-18 OBJECT AK
NORAD 100916
0.252 0.00 7.0e-05
2026-10-19 23:39:53 ICEYE-X85
NORAD 100914
TRANSPORTER-18 OBJECT AK
NORAD 100916
1.949 0.00 7.0e-05
2026-10-20 01:14:28 ICEYE-X85
NORAD 100914
TRANSPORTER-18 OBJECT AK
NORAD 100916
3.742 0.01 7.0e-05
2026-10-20 03:05:37 LEMUR-2-UNTITLED-SC
NORAD 63351
ICEYE-X85
NORAD 100914
4.712 11.06 1.4e-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