View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 42986U 26145.65108603 +.00000000 +00000-0 +15846-3 0 00006
2 42986 97.4993 159.7136 0065549 306.4444 53.0746 14.95351733 04
| Epoch (UTC): | 25 May 2026 15:37:33 |
| Eccentricity: | 0.0065549 |
| inclination: | 97.4993° |
| perigee height: | 536 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 159.7136° |
| argument of perigee: | 306.4444° |
| revolutions per day: | 14.95351733 |
| mean anomaly at epoch: | 53.0746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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