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 68076U 26145.37666466 +.00000000 +00000-0 +46963-3 0 00003
2 68076 53.1585 182.0054 0001165 62.1306 297.9815 15.34399309 04
| Epoch (UTC): | 25 May 2026 09:02:23 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 182.0054° |
| argument of perigee: | 62.1306° |
| revolutions per day: | 15.34399309 |
| mean anomaly at epoch: | 297.9815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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