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ARVAKER-2

In orbit NORAD 64567 JPUR-4323-3352-2895-8278

Observations 0
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Falcon 9 Block 5 | Transporter 14 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ARVAKER-2
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 14 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
582.49 km
Apogee
582.97 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6960.9 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:58 UTC
Two-line elements (TLE)
1 64567U 25135AR  26283.58610360  .00002036  00000-0  19676-3 0  9997
2 64567  97.7836  36.5520 0000307   7.2959 352.8265 14.93926176 71101
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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 08:10:48 ARVAKER-2
NORAD 64567 		FENGYUN 1C DEB
NORAD 32432 		5.000 9.57 1.4e-07
2026-10-11 18:30:55 ICEYE-X50
NORAD 63255 		ARVAKER-2
NORAD 64567 		3.816 13.91 1.5e-07
2026-10-11 18:36:46 ARVAKER-2
NORAD 64567 		CZ-4C R/B
NORAD 68761 		4.955 3.92 1.7e-07
2026-10-12 00:23:37 PERSEUS-M2
NORAD 40037 		ARVAKER-2
NORAD 64567 		1.964 14.76 4.5e-07
2026-10-13 00:52:26 ARVAKER-2
NORAD 64567 		NOAA 16 DEB
NORAD 41156 		2.071 14.91 3.8e-07
2026-10-13 17:55:27 ARVAKER-2
NORAD 64567 		ICEYE-X78
NORAD 68995 		4.932 14.19 8.5e-08
2026-10-14 01:15:26 ARVAKER-2
NORAD 64567 		OBJECT B
NORAD 100956 		4.787 2.20 1.9e-07
2026-10-14 02:02:53 ARVAKER-2
NORAD 64567 		CZ-6A DEB
NORAD 61402 		2.973 9.43 4.0e-07
2026-10-14 04:06:32 ARVAKER-2
NORAD 64567 		NOAA 16 DEB
NORAD 42427 		2.614 14.96 2.3e-07
2026-10-14 05:14:32 ARVAKER-2
NORAD 64567 		CZ-2C R/B
NORAD 58499 		4.042 0.41 2.7e-07
2026-10-14 10:18:42 ARVAKER-2
NORAD 64567 		KUIPER-00554
NORAD 69619 		1.969 14.01 5.6e-07
2026-10-14 19:47:17 ARVAKER-2
NORAD 64567 		CZ-2D DEB
NORAD 43487 		2.245 12.32 5.6e-07
2026-10-15 21:21:13 ARVAKER-2
NORAD 64567 		RAFS
NORAD 69923 		4.228 14.34 1.1e-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.

All conjunctions of this satellite