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WASEDA-SAT-ZERO-II

In orbit NORAD 68797 HFCT-6543-1597-0098-9086 Japan

Time in UTC

23:24

Next pass · Индия · 9°

13.10 01:15

Scheduled · JHR

84

Observations over 30 days

3%

Successful observations

19

Frames, latest 2026-10-07 15:03 UTC

Mission information
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
Electron
Spaceport
Rocket Lab Launch Complex 1A
Launch time
2026-04-23 00:03:09
Separation time
Last observers
Observer
Time of receipt
2026-10-07 15:03:38 UTC
2026-10-07 00:26:51 UTC
2026-10-06 02:13:41 UTC
2026-10-01 23:34:11 UTC
2026-09-22 17:05:28 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
522.87 km
Apogee
545.04 km
Inclination
97.5°
Period
95.4 min
Semi-major axis
6912.0 km
Velocity
7.6 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:37 UTC
Two-line elements (TLE)
1 68797U 26088F   26284.91435444  .00006616  00000-0  41248-3 0  9998
2 68797 97.5220 71.8982 0015900 41.8548 318.3893 15.09763570 25908
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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
2026-10-12 23:50:29 GLOBAL-2
NORAD 43812
WASEDA-SAT-ZERO-II
NORAD 68797
2.354 12.74 4.9e-07
2026-10-13 05:24:37 GLOBAL-2
NORAD 43812
WASEDA-SAT-ZERO-II
NORAD 68797
1.712 12.69 9.2e-07
2026-10-14 17:10:47 WASEDA-SAT-ZERO-II
NORAD 68797
CZ-2C R/B
NORAD 67475
1.254 10.91 2.1e-06
2026-10-14 21:54:38 OBJECT D
NORAD 62732
WASEDA-SAT-ZERO-II
NORAD 68797
3.208 2.97 4.2e-07
2026-10-15 02:19:42 MONOLITH
NORAD 49052
WASEDA-SAT-ZERO-II
NORAD 68797
4.265 13.99 1.2e-07
2026-10-15 05:05:55 WASEDA-SAT-ZERO-II
NORAD 68797
CZ-6A DEB
NORAD 55201
0.956 5.67 4.5e-06
2026-10-15 09:52:28 OBJECT E
NORAD 66997
WASEDA-SAT-ZERO-II
NORAD 68797
1.739 8.85 1.2e-06
2026-10-15 12:57:54 WASEDA-SAT-ZERO-II
NORAD 68797
SL-8 DEB
NORAD 6065
2.682 13.90 3.1e-07
2026-10-16 00:04:41 WASEDA-SAT-ZERO-II
NORAD 68797
CZ-2C DEB
NORAD 39204
3.045 13.99 2.3e-07
2026-10-16 05:29:23 GARAI-B (UNAMUNO)
NORAD 68463
WASEDA-SAT-ZERO-II
NORAD 68797
4.097 15.02 9.6e-08
2026-10-16 13:33:25 WASEDA-SAT-ZERO-II
NORAD 68797
COSMOS 2251 DEB
NORAD 35898
3.046 6.33 4.4e-07
2026-10-18 06:55:05 WASEDA-SAT-ZERO-II
NORAD 68797
METEOR 2-5 DEB
NORAD 38275
4.071 15.20 8.9e-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