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

ICEYE-X38

In orbit NORAD 59100 NIPW-8425-7001-2213-0488 Finland

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ICEYE-X38
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
2024-03-04 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
519.47 km
Apogee
524.27 km
Inclination
97.9°
Period
95.1 min
Semi-major axis
6900.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:43 UTC
Two-line elements (TLE)
1 59100U 24043C   26284.29394345  .00006606  00000-0  37050-3 0  9995
2 59100 97.8561 71.4303 0003482 62.3573 297.8011 15.13720537129233
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
2026-10-12 07:13:20 ICEYE-X38
NORAD 59100
PEGASUS DEB
NORAD 24091
3.508 15.22 1.2e-07
2026-10-12 08:48:43 ICEYE-X38
NORAD 59100
PEGASUS DEB
NORAD 24091
3.533 15.22 1.2e-07
2026-10-12 08:49:06 ICEYE-X38
NORAD 59100
CZ-4C DEB
NORAD 43266
1.117 5.62 3.3e-06
2026-10-12 19:55:51 ICEYE-X38
NORAD 59100
YUNYAO-1 43
NORAD 63344
3.146 4.36 4.3e-07
2026-10-12 23:28:39 HXMT (HUIYAN)
NORAD 42758
ICEYE-X38
NORAD 59100
3.465 14.30 1.7e-07
2026-10-13 10:14:13 ICEYE-X38
NORAD 59100
LEMUR-2-AHMED-ASRAR
NORAD 60576
3.665 7.64 2.9e-07
2026-10-13 12:09:42 ICEYE-X38
NORAD 59100
CZ-2D R/B
NORAD 65853
4.564 13.90 1.1e-07
2026-10-13 13:25:37 ICEYE-X38
NORAD 59100
PEGASUS DEB
NORAD 24091
4.025 15.21 9.1e-08
2026-10-13 15:01:00 ICEYE-X38
NORAD 59100
PEGASUS DEB
NORAD 24091
3.133 15.21 1.5e-07
2026-10-13 15:03:36 STARLINK-5180
NORAD 55318
ICEYE-X38
NORAD 59100
1.229 11.82 6.0e-05
2026-10-14 13:01:17 ICEYE-X38
NORAD 59100
SHIJIAN-30A (SJ-30A)
NORAD 66545
3.682 11.51 2.3e-07
2026-10-15 00:07:37 ICEYE-X38
NORAD 59100
SHIJIAN-30B (SJ-30B)
NORAD 66546
4.863 11.69 1.3e-07
2026-10-15 00:18:46 ICEYE-X38
NORAD 59100
LEMUR-2-SIERRINI
NORAD 60579
2.089 7.98 8.8e-07
2026-10-15 12:32:51 ICEYE-X38
NORAD 59100
COSMOS 2251 DEB
NORAD 37084
0.507 15.17 5.8e-06
2026-10-16 03:16:58 ICEYE-X38
NORAD 59100
OBJECT H
NORAD 100136
3.426 8.32 3.2e-07
2026-10-17 00:42:46 ICEYE-X38
NORAD 59100
OBJECT A
NORAD 67248
2.616 10.91 4.8e-07
2026-10-17 01:53:11 ICEYE-X38
NORAD 59100
FALCON 9 DEB
NORAD 48608
4.021 14.70 1.1e-07
2026-10-17 12:13:54 ICEYE-X38
NORAD 59100
SPACEMOBILE-010
NORAD 69591
1.860 5.93 1.2e-06
2026-10-17 14:36:45 ICEYE-X38
NORAD 59100
SPACEMOBILE-010
NORAD 69591
0.284 5.94 5.1e-05

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