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PARUS-6U1

In orbit NORAD 68456 SXGC-2824-2222-8971-3473 Taiwan

Time in UTC

84

Observations over 30 days

13%

Successful observations

6k

Frames, latest 2026-10-11 12:56 UTC

Mission information
Spacecraft name
PARUS-6U1
Other names
PARUS-T3
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
2026-03-29 00:00:00
Separation time
2026-03-29 00:00:00
Last observers
Observer
Time of receipt
2026-09-25 00:16:10 UTC
2026-06-28 00:36:09 UTC
2026-06-05 11:03:57 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
502.70 km
Apogee
511.62 km
Inclination
97.5°
Period
94.8 min
Semi-major axis
6885.3 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:46 UTC
Two-line elements (TLE)
1 68456U 26067AS  26284.13456452  .00007442  00000-0  36320-3 0  9996
2 68456 97.4705 240.8887 0006482 37.4055 322.7629 15.18560191 29520
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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 05:16:49 STARLINK-3866
NORAD 52500
PARUS-6U1
NORAD 68456
4.826 12.11 3.8e-06
2026-10-13 08:31:14 STARLINK-6065
NORAD 56812
PARUS-6U1
NORAD 68456
2.052 12.45 2.0e-05
2026-10-14 04:19:10 OBJECT AB
NORAD 67273
PARUS-6U1
NORAD 68456
4.238 12.77 1.5e-07
2026-10-14 05:56:31 PARUS-6U1
NORAD 68456
UNKNOWN
NORAD 270100
4.580 4.74 2.0e-07
2026-10-15 02:27:15 CO3D 2
NORAD 64902
PARUS-6U1
NORAD 68456
3.508 13.08 2.1e-07
2026-10-15 02:27:36 TRANSPORTER-15 OBJECT L
NORAD 66676
PARUS-6U1
NORAD 68456
1.210 12.69 1.9e-06
2026-10-16 06:10:54 PARUS-6U1
NORAD 68456
SL-8 R/B
NORAD 20775
4.588 15.10 3.7e-07
2026-10-16 21:03:06 PARUS-6U1
NORAD 68456
CZ-6A DEB
NORAD 54888
3.867 14.81 1.2e-07
2026-10-17 11:48:32 PARUS-6U1
NORAD 68456
PEGASUS DEB
NORAD 24091
4.045 2.06 2.7e-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