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DEKART

In orbit NORAD 46493 LBLF-9256-3450-0417-4224 Russia

Time in UTC

—

No observations scheduled

143

Observations over 30 days

58%

Successful observations

11k

Frames, latest 2026-10-09 16:31 UTC

Mission information
Spacecraft name
DEKART
Call sign
-
Network
УниверСат
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
Separation time
Last observers
Observer
Time of receipt
2026-10-04 16:16:58 UTC
2026-10-03 04:44:31 UTC
2026-10-02 05:19:53 UTC
2026-09-30 15:37:38 UTC
2026-09-30 14:06:07 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
438.98 km
Apogee
448.87 km
Inclination
97.9°
Period
93.5 min
Semi-major axis
6822.0 km
Velocity
7.65 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:02 UTC
Two-line elements (TLE)
1 46493U 20068H   26285.98997454  .00011000  00000-0  28026-3 0  9993
2 46493 97.8720 303.9169 0007321 215.4634 144.6124 15.39722100333887
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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
2026-10-14 13:13:06 DEKART
NORAD 46493
STARLINK-37920
NORAD 100489
4.968 14.79 2.2e-06
2026-10-17 06:35:48 DEKART
NORAD 46493
STARLINK-2109
NORAD 47388
4.244 14.68 3.1e-06
2026-10-18 02:41:41 DEKART
NORAD 46493
OBJECT BE
NORAD 61787
4.233 14.62 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