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KNACKSAT-2

In orbit NORAD 67683 SCWJ-8858-4107-1493-6553 Thailand

Time in UTC

—

No observations scheduled

1

Observations over 30 days

33%

Successful observations

1k

Frames, latest 2026-10-03 23:05 UTC

Mission information
Spacecraft name
KNACKSAT-2
Deployer
XSKZ-5603-1870-9019-3066
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
2025-10-21 00:01:59
Separation time
Last observers
Observer
Time of receipt
2026-08-19 05:25:20 UTC
2026-08-19 03:49:10 UTC
2026-08-19 02:10:42 UTC
2026-08-18 06:24:58 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
345.03 km
Apogee
357.25 km
Inclination
51.6°
Period
91.5 min
Semi-major axis
6729.1 km
Velocity
7.7 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 06:09:05 UTC
Two-line elements (TLE)
1 67683U 98067YA  26286.87231220  .00099368  00000-0  70849-3 0  9995
2 67683 51.6263 52.2879 0009058 296.8790 63.1282 15.72963620 38870
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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
2026-10-16 08:36:21 STARLINK-11361
NORAD 61585
KNACKSAT-2
NORAD 67683
4.020 10.06 6.5e-06
2026-10-17 00:26:56 STARLINK-11513
NORAD 62589
KNACKSAT-2
NORAD 67683
2.795 11.21 1.2e-05
2026-10-17 16:45:11 STARLINK-11390
NORAD 61947
KNACKSAT-2
NORAD 67683
1.051 3.75 1.2e-04
2026-10-18 11:38:03 STARLINK-11431
NORAD 62890
KNACKSAT-2
NORAD 67683
0.740 9.28 2.0e-04
2026-10-18 12:23:45 STARLINK-11431
NORAD 62890
KNACKSAT-2
NORAD 67683
4.512 9.29 5.4e-06
2026-10-18 13:55:11 STARLINK-11431
NORAD 62890
KNACKSAT-2
NORAD 67683
2.762 9.29 1.4e-05
2026-10-19 06:57:29 STARLINK-11433
NORAD 62008
KNACKSAT-2
NORAD 67683
4.668 0.64 6.1e-06
2026-10-19 08:58:01 KNACKSAT-2
NORAD 67683
STARLINK-38323
NORAD 100518
4.743 3.07 5.8e-06

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