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WNISAT 1R

In orbit NORAD 42835 MEKY-8319-6950-9473-3414 Japan

2017

Launch

3

Observations all time

Mission information
Spacecraft name
WNISAT 1R
Other names
Weather News Inc. Satellite 1R
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2017-07-14 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
549.66 km
Apogee
564.66 km
Inclination
97.5°
Period
95.9 min
Semi-major axis
6935.3 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:36 UTC
Two-line elements (TLE)
1 42835U 17042L   26283.94645767  .00002212  00000-0  17223-3 0  9990
2 42835 97.4971 76.0176 0010816 97.4070 262.8384 15.02182761503881
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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 06:14:51 WNISAT 1R
NORAD 42835
LEMUR-2-EMERSONROSE
NORAD 63261
3.257 11.45 2.9e-07
2026-10-12 08:40:50 WNISAT 1R
NORAD 42835
PSLV R/B
NORAD 43620
4.995 2.56 1.7e-07
2026-10-12 12:35:36 WNISAT 1R
NORAD 42835
STARLINK-34664
NORAD 64806
4.866 13.71 2.9e-06
2026-10-12 15:40:37 WNISAT 1R
NORAD 42835
ICEYE-X71
NORAD 68494
2.519 14.87 2.6e-07
2026-10-12 17:16:35 WNISAT 1R
NORAD 42835
ICEYE-X71
NORAD 68494
4.524 14.87 8.1e-08
2026-10-12 23:50:09 WNISAT 1R
NORAD 42835
PEGASUS DEB
NORAD 25445
2.917 10.52 3.9e-07
2026-10-13 03:09:13 WNISAT 1R
NORAD 42835
STARLINK-35864
NORAD 67081
3.026 12.34 9.3e-06
2026-10-13 09:22:41 WNISAT 1R
NORAD 42835
STARLINK-36221
NORAD 67215
4.387 11.16 5.0e-06
2026-10-13 09:36:22 WNISAT 1R
NORAD 42835
STARLINK-5274
NORAD 55395
3.004 14.75 5.8e-06
2026-10-13 15:05:10 WNISAT 1R
NORAD 42835
PICO-02A021
NORAD 60538
1.370 9.07 1.9e-06
2026-10-14 02:17:35 WNISAT 1R
NORAD 42835
CZ-4 DEB
NORAD 35375
2.135 11.83 6.6e-07
2026-10-14 04:43:57 WNISAT 1R
NORAD 42835
STARLINK-5284
NORAD 55297
3.138 12.78 8.2e-06
2026-10-14 09:33:24 WNISAT 1R
NORAD 42835
STARLINK-35966
NORAD 66821
2.971 8.52 1.3e-05
2026-10-14 14:22:00 WNISAT 1R
NORAD 42835
STARLINK-5074
NORAD 55438
4.012 14.64 3.4e-06
2026-10-14 15:37:04 WNISAT 1R
NORAD 42835
HAWK-9C
NORAD 59448
2.610 9.25 5.3e-07
2026-10-14 19:07:17 WNISAT 1R
NORAD 42835
STARLINK-36159
NORAD 67079
3.525 11.91 7.2e-06
2026-10-14 20:43:12 WNISAT 1R
NORAD 42835
STARLINK-36202
NORAD 67094
3.103 11.89 9.3e-06
2026-10-15 07:44:17 WNISAT 1R
NORAD 42835
STARLINK-5986
NORAD 56452
3.771 13.68 4.9e-06
2026-10-15 22:19:42 WNISAT 1R
NORAD 42835
STARLINK-5605
NORAD 55411
3.986 14.50 3.6e-06
2026-10-16 09:27:03 WNISAT 1R
NORAD 42835
AIST-1 (RS41)
NORAD 39492
4.434 9.05 1.9e-07
2026-10-16 11:57:49 WNISAT 1R
NORAD 42835
CZ-6A DEB
NORAD 61818
2.253 15.13 3.0e-07
2026-10-16 14:11:39 WNISAT 1R
NORAD 42835
SICH-1
NORAD 23657
4.009 14.78 1.4e-06
2026-10-16 15:01:50 WNISAT 1R
NORAD 42835
LEMUR-2-STARLIGHT
NORAD 66783
4.905 10.21 1.4e-07
2026-10-17 14:05:51 WNISAT 1R
NORAD 42835
STARLINK-5455
NORAD 55668
4.818 12.98 3.4e-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