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YAM-6

In orbit NORAD 59126 ZRKV-0117-0867-0214-6594

Observations 1
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2024

Falcon 9 Block 5 | Transporter 10 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

1

Observations all time

Mission information
Spacecraft name
YAM-6
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Transporter 10 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2024-03-04 22:05:00
Separation time
2024-03-04 23:11:26
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
440.86 km
Apogee
452.11 km
Inclination
97.6°
Period
93.6 min
Semi-major axis
6824.6 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:38 UTC
Two-line elements (TLE)
1 59126U 24043AE  26283.92575713  .00012485  00000-0  32678-3 0  9995
2 59126  97.5725  68.5612 0008241 165.6672 194.4808 15.38839203145103
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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 18:38:04 STARLINK-4166
NORAD 53291 		YAM-6
NORAD 59126 		4.787 14.58 2.5e-06
2026-10-11 23:46:34 STARLINK-1047
NORAD 44752 		YAM-6
NORAD 59126 		2.678 14.10 9.2e-06
2026-10-12 05:04:39 YAM-6
NORAD 59126 		STARLINK-38259
NORAD 100252 		3.993 11.66 5.8e-06
2026-10-12 06:38:50 YAM-6
NORAD 59126 		STARLINK-38136
NORAD 100166 		4.836 12.56 3.6e-06
2026-10-12 20:49:38 STARLINK-2109
NORAD 47388 		YAM-6
NORAD 59126 		4.079 9.20 6.6e-06
2026-10-12 22:22:09 YAM-6
NORAD 59126 		STARLINK-37550
NORAD 100277 		4.329 10.64 5.4e-06
2026-10-13 04:37:24 YAM-6
NORAD 59126 		STARLINK-37397
NORAD 100411 		3.529 13.53 5.9e-06
2026-10-13 18:39:12 STARLINK-3725
NORAD 52123 		YAM-6
NORAD 59126 		4.370 11.13 5.1e-06
2026-10-14 13:33:37 YAM-6
NORAD 59126 		STARLINK-37650
NORAD 100056 		4.874 14.75 2.3e-06
2026-10-16 01:27:15 STARLINK-3588
NORAD 51869 		YAM-6
NORAD 59126 		4.322 5.90 6.7e-06
2026-10-16 15:23:15 STARLINK-4006
NORAD 52676 		YAM-6
NORAD 59126 		4.698 14.37 2.8e-06

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