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VINDLER 2.3

In orbit NORAD 68486 AKPG-5053-0001-7320-2859

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
VINDLER 2.3
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
587.15 km
Apogee
588.51 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6966.0 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:37 UTC
Two-line elements (TLE)
1 68486U 26067BY  26284.65879214  .00001409  00000-0  14355-3 0  9992
2 68486 97.7723 241.2212 0000964 50.0476 310.0827 14.92288485 29096
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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 06:08:46 VINDLER 2.3
NORAD 68486
ISIS 1 DEB
NORAD 36301
3.678 15.44 1.1e-07
2026-10-13 14:54:05 VINDLER 2.3
NORAD 68486
IRIDE-MS2-HEO-14
NORAD 68986
1.629 7.66 1.5e-06
2026-10-14 11:29:42 VINDLER 2.3
NORAD 68486
THOR ABLESTAR DEB
NORAD 15783
3.488 14.99 1.3e-07
2026-10-15 09:16:57 VINDLER 2.3
NORAD 68486
N1-ATLAS
NORAD 68501
4.260 0.00 1.1e-07
2026-10-15 10:15:13 VINDLER 2.3
NORAD 68486
N1-ATLAS
NORAD 68501
3.709 0.01 3.2e-07
2026-10-15 10:53:35 VINDLER 2.3
NORAD 68486
CZ-4B DEB
NORAD 35331
4.336 14.90 8.7e-08
2026-10-15 15:49:03 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
4.203 14.64 1.0e-07
2026-10-15 17:25:37 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
2.283 14.64 3.4e-07
2026-10-15 19:02:11 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
0.759 14.64 3.1e-06
2026-10-15 19:10:51 LEMUR-2-SEJONG-3
NORAD 68482
VINDLER 2.3
NORAD 68486
4.997 0.04 1.8e-07
2026-10-15 20:38:44 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
1.935 14.64 4.8e-07
2026-10-15 22:15:18 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
3.836 14.64 1.2e-07
2026-10-15 23:03:35 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
3.409 14.67 1.5e-07
2026-10-16 00:40:09 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
1.613 14.67 6.9e-07
2026-10-16 01:01:41 VINDLER 2.3
NORAD 68486
FENGYUN 1C DEB
NORAD 32137
4.435 14.87 8.5e-08
2026-10-16 02:16:43 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
1.185 14.67 1.3e-06
2026-10-16 03:53:17 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
2.832 14.67 2.2e-07
2026-10-16 05:29:50 IRIDE-MS2-HEO-3
NORAD 64568
VINDLER 2.3
NORAD 68486
4.738 14.67 8.0e-08
2026-10-16 07:37:27 SHIYAN-30 01
NORAD 65851
VINDLER 2.3
NORAD 68486
3.968 7.94 2.4e-07
2026-10-16 11:55:45 HUBBLE 7
NORAD 64592
VINDLER 2.3
NORAD 68486
2.728 14.69 2.4e-07
2026-10-17 21:42:22 VINDLER 2.3
NORAD 68486
TIUNGSAT-1 (MO-46)
NORAD 26548
2.895 14.55 7.9e-08

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