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 68650U 26144.79050773 +.00000000 +00000-0 +36093-4 0 00008
2 68650 88.9876 323.3976 0010795 74.9929 285.2427 13.70216349 04
| Epoch (UTC): | 24 May 2026 18:58:19 |
| Eccentricity: | 0.0010795 |
| inclination: | 88.9876° |
| perigee height: | 991 km |
| apogee height: | 1007 km |
| right ascension of ascending node: | 323.3976° |
| argument of perigee: | 74.9929° |
| revolutions per day: | 13.70216349 |
| mean anomaly at epoch: | 285.2427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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