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QPS-SAR-8

In orbit NORAD 60542 XOCE-2797-1055-8900-9065

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
QPS-SAR-8
Other names
QPS-SAR-8 AMATERU-IV
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
2024-08-16 18:56:00
Separation time
2024-08-16 21:32:08
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
545.43 km
Apogee
551.25 km
Inclination
97.7°
Period
95.7 min
Semi-major axis
6926.5 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:19 UTC
Two-line elements (TLE)
1 60542U 24149CC  26282.64625428  .00004993  00000-0  35560-3 0  9991
2 60542 97.6583 0.8596 0004196 87.5385 272.6321 15.05052913117486
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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 09:43:40 YAOGAN-30 10C
NORAD 48863
QPS-SAR-8 (AMATERU-IV)
NORAD 60542
4.171 13.76 1.3e-07
2026-10-11 15:23:41 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
STRIX-10
NORAD 100746
4.007 14.05 1.3e-07
2026-10-12 10:16:49 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
DELFI-N3XT
NORAD 39428
3.139 14.74 1.8e-07
2026-10-12 11:43:54 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
CZ-4B R/B
NORAD 37181
0.857 3.84 5.8e-06
2026-10-13 22:37:08 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
ELECTRON KICK STAGE R/B
NORAD 69178
3.354 10.41 3.0e-07
2026-10-14 04:20:23 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
STARLINK-34988
NORAD 65453
4.827 13.67 3.0e-06
2026-10-14 08:59:35 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
ELECTRON KICK STAGE R/B
NORAD 69178
3.313 10.61 3.0e-07
2026-10-15 18:16:16 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
STRIX-9
NORAD 100561
4.988 14.03 8.7e-08
2026-10-16 23:08:22 QPS-SAR-8 (AMATERU-IV)
NORAD 60542
FENGYUN 1C DEB
NORAD 30912
2.507 15.00 2.6e-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