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TeikyoSat-4

In orbit NORAD 49396 UYHX-6974-4483-5549-8559 Japan

2021

Launch

3

Observations all time

Mission information
Spacecraft name
TeikyoSat-4
Other names
JS1YHH, Ooruri, TS-4
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2021-11-09 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
526.45 km
Apogee
540.85 km
Inclination
97.4°
Period
95.4 min
Semi-major axis
6911.8 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:02 UTC
Two-line elements (TLE)
1 49396U 21102B   26287.29378946  .00001778  00000-0  11355-3 0  9991
2 49396 97.3593 312.1258 0010461 238.6680 121.3526 15.09847499270696
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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
2026-10-15 03:42:17 TEIKYOSAT-4 (OORURI)
NORAD 49396
COSMOS 252 DEB
NORAD 18431
2.359 15.25 3.0e-07
2026-10-15 08:05:06 TEIKYOSAT-4 (OORURI)
NORAD 49396
OBJECT H
NORAD 67000
4.323 6.42 2.2e-07
2026-10-15 10:28:17 TEIKYOSAT-4 (OORURI)
NORAD 49396
OBJECT H
NORAD 67000
3.908 6.42 2.7e-07
2026-10-15 19:30:46 TEIKYOSAT-4 (OORURI)
NORAD 49396
CZ-4B R/B
NORAD 38039
3.896 14.98 1.1e-07
2026-10-16 08:09:13 COSMO-SKYMED 3
NORAD 33412
TEIKYOSAT-4 (OORURI)
NORAD 49396
1.587 14.90 6.6e-07
2026-10-16 17:25:16 TEIKYOSAT-4 (OORURI)
NORAD 49396
STARLINK-5317
NORAD 55283
2.111 12.43 1.9e-05
2026-10-17 07:20:38 TEIKYOSAT-4 (OORURI)
NORAD 49396
UNKNOWN
NORAD 82180
2.258 15.10 3.2e-07
2026-10-17 14:52:39 TEIKYOSAT-4 (OORURI)
NORAD 49396
STARLINK-36215
NORAD 67100
2.966 14.26 7.1e-06
2026-10-17 21:31:39 TEIKYOSAT-4 (OORURI)
NORAD 49396
TLV R/B
NORAD 58501
4.214 11.92 1.7e-07
2026-10-18 15:41:59 TEIKYOSAT-4 (OORURI)
NORAD 49396
COSMOS 2251 DEB
NORAD 37496
0.134 11.03 1.8e-04
2026-10-18 19:37:03 COSMOS 2494 (SKRL-756 2)
NORAD 39491
TEIKYOSAT-4 (OORURI)
NORAD 49396
1.891 15.15 4.2e-07
2026-10-19 00:04:49 TEIKYOSAT-4 (OORURI)
NORAD 49396
FENGYUN 1C DEB
NORAD 31231
2.582 15.03 2.4e-07
2026-10-19 16:49:03 TEIKYOSAT-4 (OORURI)
NORAD 49396
EROS C3
NORAD 54880
1.316 6.81 2.3e-06
2026-10-19 19:51:42 TEIKYOSAT-4 (OORURI)
NORAD 49396
IXPE
NORAD 49954
2.948 11.43 3.6e-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