ARVAKER-3
In orbit NORAD 64566 KYID-1980-2687-0794-7123
Falcon 9 Block 5
Carrier rocket
Space Launch Complex 4E
Spaceport
0
Observations all time
The satellite is in orbit
The network has not received data from this satellite for a long time
Gallery
1 64566U 25135AQ 26283.90673145 .00002170 00000-0 20893-3 0 9994
2 64566 97.7824 36.8314 0000480 294.5152 65.6018 14.93993500 71154
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 |
|---|---|---|---|---|---|
| 2026-10-11 18:25:15 |
ARVAKER-3
NORAD 64566 |
TIROS 6
NORAD 397 |
4.073 | 13.88 | 1.1e-07 |
| 2026-10-12 01:22:01 |
ARVAKER-3
NORAD 64566 |
DELTA 1 DEB
NORAD 26036 |
4.508 | 14.33 | 9.8e-08 |
| 2026-10-16 11:34:48 |
ARVAKER-3
NORAD 64566 |
TRANSPORTER-14 OBJECT BQ
NORAD 64590 |
3.604 | 0.05 | 3.4e-07 |
| 2026-10-16 12:22:48 |
ARVAKER-3
NORAD 64566 |
TRANSPORTER-14 OBJECT BQ
NORAD 64590 |
4.626 | 0.05 | 2.1e-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.
