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ICEYE-X2

In orbit NORAD 43800 NSPV-9593-9175-6289-3371 Finland

Observations 0
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2018

Falcon 9 Block 5 | Spaceflight SSO-A

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X2
Other names
2018-099AU
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 | Spaceflight SSO-A
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2018-12-03 00:00:00
Separation time
2018-12-03 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
499.66 km
Apogee
511.14 km
Inclination
97.4°
Period
94.8 min
Semi-major axis
6883.5 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:55 UTC
Two-line elements (TLE)
1 43800U 18099AU  26283.60205109  .00014757  00000-0  70387-3 0  9998
2 43800  97.4230 335.4260 0008277 258.2954 101.7352 15.19155333430332
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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
2026-10-11 12:25:35 ICEYE-X2
NORAD 43800 		YAOGAN-39 05C
NORAD 58559 		2.572 11.80 4.6e-07
2026-10-11 15:20:30 ICEYE-X2
NORAD 43800 		FLOCK 4H-25
NORAD 66728 		1.978 2.64 1.1e-06
2026-10-12 11:04:16 ICEYE-X2
NORAD 43800 		RASSVET-3 9
NORAD 68368 		4.595 10.34 1.6e-07
2026-10-12 16:46:38 ICEYE-X2
NORAD 43800 		SNAPPY
NORAD 69014 		1.101 14.74 1.5e-06
2026-10-12 21:55:10 ICEYE-X2
NORAD 43800 		TITAN 3C TRANSTAGE DEB
NORAD 1961 		4.068 11.42 1.9e-07
2026-10-12 23:30:00 ICEYE-X2
NORAD 43800 		TITAN 3C TRANSTAGE DEB
NORAD 1961 		3.912 11.45 2.0e-07
2026-10-13 01:52:16 ICEYE-X2
NORAD 43800 		TITAN 3C TRANSTAGE DEB
NORAD 1961 		4.481 11.48 1.5e-07
2026-10-13 05:16:01 ICEYE-X2
NORAD 43800 		BRO-18
NORAD 64550 		4.351 7.81 2.0e-07
2026-10-13 08:19:42 ICEYE-X2
NORAD 43800 		COSMOS 2251 DEB
NORAD 40797 		4.612 14.98 7.7e-08
2026-10-13 15:26:15 ICEYE-X2
NORAD 43800 		COSMOS 2251 DEB
NORAD 40797 		3.182 14.99 1.6e-07
2026-10-13 17:01:04 ICEYE-X2
NORAD 43800 		COSMOS 2251 DEB
NORAD 40797 		3.307 15.00 1.5e-07
2026-10-14 20:00:41 ICEYE-X2
NORAD 43800 		AC1-002
NORAD 66745 		4.407 2.53 2.2e-07
2026-10-15 11:51:35 ICEYE-X2
NORAD 43800 		BESSA
NORAD 68836 		4.202 11.10 1.8e-07
2026-10-15 11:54:22 ICEYE-X2
NORAD 43800 		STARLINK-5862
NORAD 55920 		3.735 12.47 6.1e-06
2026-10-15 14:13:50 ICEYE-X2
NORAD 43800 		BESSA
NORAD 68836 		0.660 11.09 7.4e-06
2026-10-16 03:13:24 ICEYE-X2
NORAD 43800 		STARLINK-4472
NORAD 53661 		2.419 15.08 8.1e-06
2026-10-16 14:25:56 ICEYE-X2
NORAD 43800 		TITAN 3C TRANSTAGE DEB
NORAD 1961 		3.922 12.58 1.8e-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