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JACK-002

In orbit NORAD 68417 KXEN-6599-9366-4098-3918 South Korea

Time in UTC

08:48

Next pass · Индия · 14°

271

Observations over 30 days

74%

Successful observations

96k

Frames, latest 2026-10-15 03:01 UTC

Mission information
Spacecraft name
JACK-002
Status
Active
The satellite is in orbit
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-30 11:02:00
Separation time
Last observers
Observer
Time of receipt
2026-10-15 03:01:15 UTC
2026-10-15 01:26:29 UTC
2026-10-15 01:26:29 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
499.69 km
Apogee
501.86 km
Inclination
97.5°
Period
94.7 min
Semi-major axis
6878.9 km
Velocity
7.61 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68417U 26067B   26287.11584371  .00007559  00000-0  34720-3 0  9997
2 68417 97.4730 244.4385 0001572 153.5361 206.5955 15.20673531 30016
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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 03:20:41 JACK-002
NORAD 68417
OUT OF THE BOX (OOTB)
NORAD 68428
4.392 0.04 2.3e-07
2026-10-16 13:33:08 BUZZER-1
NORAD 62609
JACK-002
NORAD 68417
2.467 12.99 4.3e-07
2026-10-16 20:40:23 JACK-002
NORAD 68417
OBJECT J
NORAD 51832
3.128 11.73 3.1e-07
2026-10-16 22:15:08 JACK-002
NORAD 68417
OBJECT J
NORAD 51832
2.993 11.73 3.4e-07
2026-10-16 23:02:32 JACK-002
NORAD 68417
OBJECT J
NORAD 51832
3.938 11.76 2.0e-07
2026-10-16 23:49:53 JACK-002
NORAD 68417
OBJECT J
NORAD 51832
4.778 11.73 1.3e-07
2026-10-17 00:37:16 JACK-002
NORAD 68417
OBJECT J
NORAD 51832
3.918 11.76 2.0e-07
2026-10-17 01:26:55 JACK-002
NORAD 68417
SL-8 R/B
NORAD 20775
3.642 15.08 5.9e-07
2026-10-17 06:12:33 ETIHAD-SAT
NORAD 63226
JACK-002
NORAD 68417
2.873 8.30 4.6e-07
2026-10-18 21:26:41 STARLINK-5925
NORAD 55945
JACK-002
NORAD 68417
1.933 15.05 1.3e-05
2026-10-18 22:14:05 STARLINK-5925
NORAD 55945
JACK-002
NORAD 68417
3.646 15.07 3.6e-06
2026-10-18 22:24:57 JACK-002
NORAD 68417
ELECTRON KICK STAGE R/B
NORAD 60085
4.313 11.73 1.6e-07
2026-10-19 00:06:02 JACK-002
NORAD 68417
COSMOS 2251 DEB
NORAD 33811
1.697 13.44 8.5e-07
2026-10-19 17:21:30 NUSAT-51 (YVONNE BRILL)
NORAD 66740
JACK-002
NORAD 68417
3.388 12.69 2.4e-07
2026-10-20 04:10:48 STARLINK-5862
NORAD 55920
JACK-002
NORAD 68417
1.523 15.11 2.0e-05

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