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 55817U 26145.40162690 +.00000000 +00000-0 +40192-3 0 00004
2 55817 87.9180 278.9719 0002337 101.7102 258.4294 13.20771828 04
| Epoch (UTC): | 25 May 2026 09:38:20 |
| Eccentricity: | 0.0002337 |
| inclination: | 87.9180° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9719° |
| argument of perigee: | 101.7102° |
| revolutions per day: | 13.20771828 |
| mean anomaly at epoch: | 258.4294° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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