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FSI-SAT2

In orbit NORAD 68792 YZDO-1863-9002-1980-6647 Japan

Time in UTC

—

No observations scheduled

5

Observations over 30 days

77%

Successful observations

1k

Frames, latest 2026-10-09 13:32 UTC

Mission information
Spacecraft name
FSI-SAT2
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Electron
Spaceport
Rocket Lab Launch Complex 1A
Launch time
2026-04-23 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-10-09 13:32:41 UTC
2026-09-19 23:19:21 UTC
2026-09-18 23:26:08 UTC
2026-09-14 23:50:41 UTC
2026-08-31 23:41:36 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
529.61 km
Apogee
551.37 km
Inclination
97.5°
Period
95.5 min
Semi-major axis
6918.6 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 68792U 26088A   26283.93485865  .00005244  00000-0  34758-3 0  9990
2 68792 97.5235 70.4732 0015723 74.0372 286.2587 15.07610875 25723
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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 11:44:11 STARLINK-4502
NORAD 53557
FSI-SAT2
NORAD 68792
2.204 12.08 1.8e-05
2026-10-11 13:34:34 FSI-SAT2
NORAD 68792
UNKNOWN
NORAD 87051
3.052 15.27 1.7e-07
2026-10-11 15:40:51 GRBBETA
NORAD 60237
FSI-SAT2
NORAD 68792
4.020 11.51 1.9e-07
2026-10-11 17:16:26 GRBBETA
NORAD 60237
FSI-SAT2
NORAD 68792
1.639 11.49 1.1e-06
2026-10-11 18:38:58 FSI-SAT2
NORAD 68792
COSMOS 2251 DEB
NORAD 34301
3.796 14.76 1.2e-07
2026-10-12 14:46:41 GRBBETA
NORAD 60237
FSI-SAT2
NORAD 68792
0.469 11.22 1.4e-05
2026-10-12 16:22:15 GRBBETA
NORAD 60237
FSI-SAT2
NORAD 68792
4.985 11.20 1.3e-07
2026-10-12 18:18:59 YAOGAN-30 11A
NORAD 49026
FSI-SAT2
NORAD 68792
4.181 13.67 1.3e-07
2026-10-12 20:15:19 FSI-SAT2
NORAD 68792
PROSPERO (BLACK ARROW)
NORAD 5580
3.551 12.97 2.1e-07
2026-10-13 01:40:34 FSI-SAT2
NORAD 68792
CZ-6A DEB
NORAD 60842
2.068 15.15 3.6e-07
2026-10-13 15:16:13 FSI-SAT2
NORAD 68792
SL-16 DEB
NORAD 39708
3.393 12.76 2.3e-07
2026-10-14 10:12:10 UWE-3
NORAD 39446
FSI-SAT2
NORAD 68792
4.366 14.98 8.4e-08
2026-10-14 14:15:20 FSI-SAT2
NORAD 68792
CZ-6A DEB
NORAD 64650
4.973 15.16 6.1e-08
2026-10-14 16:29:29 FSI-SAT2
NORAD 68792
COSMOS 2251 DEB
NORAD 37084
4.226 15.12 8.4e-08
2026-10-15 15:55:17 OBJECT E
NORAD 62733
FSI-SAT2
NORAD 68792
4.538 3.02 2.1e-07
2026-10-16 04:34:29 FSI-SAT2
NORAD 68792
SL-16 DEB
NORAD 22296
2.149 14.44 4.3e-07
2026-10-16 04:44:03 FSI-SAT2
NORAD 68792
CZ-4B DEB
NORAD 36290
4.535 13.25 1.2e-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