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 68899U 26145.58335647 +.00000000 +00000-0 -56486-1 0 00003
2 68899 97.2845 341.3593 0001843 66.3857 70.7080 15.42751567 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001843 |
| inclination: | 97.2845° |
| perigee height: | 437 km |
| apogee height: | 439 km |
| right ascension of ascending node: | 341.3593° |
| argument of perigee: | 66.3857° |
| revolutions per day: | 15.42751567 |
| mean anomaly at epoch: | 70.7080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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