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ARVAKER I

In orbit NORAD 63252 GGXJ-9238-8176-9137-9636

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
ARVAKER I
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
2025-03-15 06:43:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
578.08 km
Apogee
581.18 km
Inclination
97.7°
Period
96.3 min
Semi-major axis
6957.7 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 63252U 25052AU  26283.42380383  .00001944  00000-0  18329-3 0  9998
2 63252 97.6699 172.1764 0002337 158.3741 201.7579 14.94926000 85827
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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
2026-10-13 02:01:44 ARVAKER-1
NORAD 63252
CZ-6A DEB
NORAD 61126
4.598 10.78 1.5e-07
2026-10-13 06:30:59 ARVAKER-1
NORAD 63252
COSMOS 249 DEB
NORAD 3790
0.500 15.15 6.6e-06
2026-10-13 11:44:50 ARVAKER-1
NORAD 63252
LEMUR-2-HUBBLE-4
NORAD 64565
3.600 13.88 1.7e-07
2026-10-13 15:07:16 ARVAKER-1
NORAD 63252
CZ-2D R/B
NORAD 68141
1.700 11.61 1.1e-06
2026-10-13 16:42:03 ARVAKER-1
NORAD 63252
CZ-6A DEB
NORAD 54927
2.779 14.87 2.2e-07
2026-10-13 23:22:31 ARVAKER-1
NORAD 63252
TITAN 4B DEB
NORAD 27469
3.421 15.02 1.3e-07
2026-10-14 05:21:30 HODOYOSHI-4
NORAD 40011
ARVAKER-1
NORAD 63252
4.972 8.54 1.5e-07
2026-10-14 12:00:12 ARVAKER-1
NORAD 63252
CZ-6A DEB
NORAD 56586
1.597 14.90 6.4e-07
2026-10-15 05:35:51 ARVAKER-1
NORAD 63252
CZ-6A DEB
NORAD 54997
2.876 14.73 2.1e-07
2026-10-15 17:48:27 ARVAKER-1
NORAD 63252
FFLY02
NORAD 65322
4.684 14.99 7.2e-08
2026-10-15 23:44:05 ARVAKER-1
NORAD 63252
FREGAT DEB
NORAD 45638
1.914 12.52 7.8e-07
2026-10-16 06:32:18 ARVAKER-1
NORAD 63252
OBJECT J
NORAD 44887
3.425 14.89 1.4e-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