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IOD2_Startical

In orbit NORAD 64538 TOTH-8884-9961-6728-7092 Spain

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
IOD2_Startical
Other names
2025-135L
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
2025-06-23 00:00:00
Separation time
2025-06-23 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
495.53 km
Apogee
503.41 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6877.6 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:20 UTC
Two-line elements (TLE)
1 64538U 25135L   26282.54093590  .00003613  00000-0  16555-3 0  9995
2 64538 97.4805 36.2039 0005732 127.6302 232.5454 15.21106338 72208
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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 09:35:38 ASNARO
NORAD 40298
IOD-2
NORAD 64538
4.786 5.26 1.8e-07
2026-10-11 10:49:57 IOD-2
NORAD 64538
COSMOS 2251 DEB
NORAD 40794
3.663 15.18 1.1e-07
2026-10-12 09:58:11 CAS500-1
NORAD 47932
IOD-2
NORAD 64538
1.907 14.12 5.9e-07
2026-10-12 13:05:22 IOD-2
NORAD 64538
COSMOS 252 DEB
NORAD 3900
3.123 11.00 3.3e-07
2026-10-13 01:19:36 YAOGAN-43 02D
NORAD 60948
IOD-2
NORAD 64538
4.444 13.29 1.3e-07
2026-10-13 01:53:38 IOD-2
NORAD 64538
FLAMINGO-1
NORAD 67391
3.527 12.80 2.2e-07
2026-10-13 14:53:51 IOD-2
NORAD 64538
IRIDIUM 5
NORAD 24795
3.196 15.25 1.2e-06
2026-10-13 18:25:52 IOD-2
NORAD 64538
IRIDE-MS1-EAGLET 2-7
NORAD 66701
4.415 5.39 2.1e-07
2026-10-14 02:27:19 IOD-2
NORAD 64538
COSMO
NORAD 68460
2.556 14.80 2.7e-07
2026-10-14 02:34:03 STARLINK-5293
NORAD 55295
IOD-2
NORAD 64538
4.424 15.10 2.4e-06
2026-10-14 03:14:42 IOD-2
NORAD 64538
COSMO
NORAD 68460
4.455 14.75 8.9e-08
2026-10-14 06:27:50 IOD-2
NORAD 64538
STPSAT-7
NORAD 68630
4.198 6.84 2.3e-07
2026-10-14 19:44:41 IOD-2
NORAD 64538
COSMOS 2251 DEB
NORAD 40797
4.898 13.94 9.3e-08
2026-10-14 22:39:44 STARLINK-3276
NORAD 50189
IOD-2
NORAD 64538
3.843 9.66 7.3e-06
2026-10-14 23:27:03 STARLINK-3276
NORAD 50189
IOD-2
NORAD 64538
3.814 9.65 7.4e-06
2026-10-15 10:35:59 LIZZIESAT-3 (LS-3)
NORAD 63233
IOD-2
NORAD 64538
2.993 13.97 2.5e-07
2026-10-15 13:50:51 IOD-2
NORAD 64538
ICEYE-X61
NORAD 66754
3.969 5.45 2.6e-07
2026-10-16 04:51:11 SNUSAT-2
NORAD 43782
IOD-2
NORAD 64538
1.976 7.78 9.9e-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