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 55931U 26145.61111705 +.00000000 +00000-0 -68743-4 0 00009
2 55931 69.9996 110.3361 0003905 267.9469 92.1243 14.98328575 01
| Epoch (UTC): | 25 May 2026 14:40:00 |
| Eccentricity: | 0.0003905 |
| inclination: | 69.9996° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 110.3361° |
| argument of perigee: | 267.9469° |
| revolutions per day: | 14.98328575 |
| mean anomaly at epoch: | 92.1243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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