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ET-001A

In orbit NORAD 69925 GXIV-3500-0804-8024-6424

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ET-001A
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
581.20 km
Apogee
591.53 km
Inclination
97.7°
Period
96.5 min
Semi-major axis
6964.5 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:57:00 UTC
Two-line elements (TLE)
1 69925U 26156BJ  26283.21127513  .00004422  00000-0  43310-3 0  9990
2 69925 97.7416 182.1312 0007507 184.8493 175.2655 14.92766206 14156
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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 05:36:12 ICEYE-X82
NORAD 68996
ET-001A
NORAD 69925
2.090 0.50 1.0e-06
2026-10-11 05:50:50 ET-001A
NORAD 69925
CZ-6A DEB
NORAD 55532
3.171 14.89 1.6e-07
2026-10-11 10:32:09 ICEYE-X52
NORAD 64572
ET-001A
NORAD 69925
1.872 14.34 5.7e-07
2026-10-11 15:49:55 ET-001A
NORAD 69925
SL-16 DEB
NORAD 22392
4.216 4.52 2.4e-07
2026-10-11 18:20:23 ET-001A
NORAD 69925
FENGYUN 1C DEB
NORAD 30016
4.018 14.53 1.2e-07
2026-10-11 23:15:41 ET-001A
NORAD 69925
SL-14 R/B
NORAD 11672
1.948 10.02 2.2e-06
2026-10-12 22:26:19 ET-001A
NORAD 69925
CZ-6A DEB
NORAD 56283
4.046 14.79 1.0e-07
2026-10-13 04:02:26 ET-001A
NORAD 69925
NOAA 12 DEB
NORAD 37831
2.451 14.87 2.8e-07
2026-10-13 11:56:11 ET-001A
NORAD 69925
NOAA 17 DEB
NORAD 48165
2.881 14.98 1.9e-07
2026-10-14 04:09:55 ET-001A
NORAD 69925
CZ-4C DEB
NORAD 37570
0.278 14.91 2.1e-05
2026-10-14 14:02:21 FOREST-19 (PATADASTRA)
NORAD 69001
ET-001A
NORAD 69925
4.453 0.46 2.2e-07
2026-10-14 15:38:52 FOREST-19 (PATADASTRA)
NORAD 69001
ET-001A
NORAD 69925
0.549 0.46 1.5e-05
2026-10-14 22:53:11 FOREST-19 (PATADASTRA)
NORAD 69001
ET-001A
NORAD 69925
2.723 0.45 5.9e-07
2026-10-15 00:29:42 FOREST-19 (PATADASTRA)
NORAD 69001
ET-001A
NORAD 69925
2.458 0.45 7.3e-07
2026-10-15 17:28:47 ET-001A
NORAD 69925
ET-001B
NORAD 69941
3.914 0.01 9.7e-05
2026-10-15 19:05:26 ET-001A
NORAD 69925
ET-001B
NORAD 69941
1.598 0.00 9.7e-05
2026-10-15 20:22:19 ET-001A
NORAD 69925
ET-001B
NORAD 69941
0.523 0.00 9.7e-05
2026-10-15 20:35:08 LEMUR-2-JULIA-JOEL
NORAD 68476
ET-001A
NORAD 69925
1.044 7.26 3.6e-06
2026-10-15 21:12:48 ET-001A
NORAD 69925
ET-001B
NORAD 69941
0.212 0.00 9.7e-05
2026-10-15 21:47:09 ET-001A
NORAD 69925
CZ-6A DEB
NORAD 56586
2.313 14.97 3.0e-07
2026-10-15 22:50:24 ET-001A
NORAD 69925
ET-001B
NORAD 69941
2.523 0.00 9.7e-05
2026-10-15 22:59:52 LEMUR-2-JULIA-JOEL
NORAD 68476
ET-001A
NORAD 69925
3.621 7.24 3.0e-07
2026-10-16 00:27:03 ET-001A
NORAD 69925
ET-001B
NORAD 69941
4.841 0.01 1.9e-07
2026-10-16 09:39:29 ET-001A
NORAD 69925
UNKNOWN
NORAD 270070
1.967 14.80 4.8e-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