QPS-SAR-7
In orbit NORAD 59447 DLUP-6316-3111-7417-6906 Japan
2024
Launch
0
Observations all time
Gallery
1 59447U 24066F 26283.91411010 .00006909 00000-0 43173-3 0 9990
2 59447 45.6051 357.3826 0002959 272.2841 87.7706 15.10165115137717
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.
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 07:11:35 |
QPS-SAR-7 (TSUKUYOMI-II)
NORAD 59447 |
OBJECT A
NORAD 59810 |
0.653 | 6.96 | 9.3e-06 |
| 2026-10-13 13:20:48 |
QPS-SAR-7 (TSUKUYOMI-II)
NORAD 59447 |
RAAF M1
NORAD 43779 |
3.154 | 6.93 | 4.0e-07 |
| 2026-10-14 01:37:40 |
STARLINK-4082
NORAD 52658 |
QPS-SAR-7 (TSUKUYOMI-II)
NORAD 59447 |
4.916 | 8.03 | 4.8e-06 |
| 2026-10-16 08:17:18 |
JILIN-1 KUANFU 01
NORAD 45016 |
QPS-SAR-7 (TSUKUYOMI-II)
NORAD 59447 |
4.612 | 7.53 | 1.8e-07 |
| 2026-10-16 11:00:48 |
QPS-SAR-7 (TSUKUYOMI-II)
NORAD 59447 |
OBJECT D
NORAD 62732 |
2.954 | 13.39 | 2.8e-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.
