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T.MicroSat-2

In orbit NORAD 68433 ZVLY-3305-1364-3664-7659 Taiwan

Time in UTC

13.10 00:24

Scheduled · Сампо-400 [R1NAV]

95

Observations over 30 days

96%

Successful observations

26k

Frames, latest 2026-10-12 00:44 UTC

Mission information
Spacecraft name
T.MicroSat-2
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-29 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-10-12 00:44:38 UTC
2026-10-11 11:52:34 UTC
2026-10-11 10:16:28 UTC
2026-10-07 11:23:45 UTC
2026-10-07 09:48:47 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
503.40 km
Apogee
512.43 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6886.1 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 68433U 26067T   26284.15199529  .00006351  00000-0  31271-3 0  9990
2 68433 97.4715 240.9054 0006555 34.0214 326.1439 15.18310863 29520
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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
2026-10-13 05:01:29 FLOCK 4H-3
NORAD 66706
T.MICROSAT-2
NORAD 68433
4.543 12.74 1.3e-07
2026-10-16 03:18:17 T.MICROSAT-2
NORAD 68433
CZ-6A DEB
NORAD 55530
4.952 14.74 7.2e-08
2026-10-16 04:33:28 T.MICROSAT-2
NORAD 68433
COSMOS 2251 DEB
NORAD 36047
3.861 15.17 1.0e-07
2026-10-16 23:58:29 SUPERVIEW NEO-1 02
NORAD 52322
T.MICROSAT-2
NORAD 68433
4.637 12.50 1.3e-07
2026-10-17 02:14:23 T.MICROSAT-2
NORAD 68433
FENGYUN 1C DEB
NORAD 33655
4.491 14.78 8.8e-08
2026-10-18 04:13:57 OBJECT B
NORAD 67747
T.MICROSAT-2
NORAD 68433
3.884 15.02 1.1e-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