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 68799U 26145.39791271 +.00000000 +00000-0 +22785-3 0 00006
2 68799 97.5025 295.3266 0020013 155.2282 204.9912 15.08600679 02
| Epoch (UTC): | 25 May 2026 09:32:59 |
| Eccentricity: | 0.0020013 |
| inclination: | 97.5025° |
| perigee height: | 527 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 295.3266° |
| argument of perigee: | 155.2282° |
| revolutions per day: | 15.08600679 |
| mean anomaly at epoch: | 204.9912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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