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 68936U 26145.49547899 +.00000000 +00000-0 +87665-3 0 00003
2 68936 51.8752 177.6541 0017679 69.9579 290.3306 15.29358318 06
| Epoch (UTC): | 25 May 2026 11:53:29 |
| Eccentricity: | 0.0017679 |
| inclination: | 51.8752° |
| perigee height: | 466 km |
| apogee height: | 490 km |
| right ascension of ascending node: | 177.6541° |
| argument of perigee: | 69.9579° |
| revolutions per day: | 15.29358318 |
| mean anomaly at epoch: | 290.3306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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