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 68616U 26145.58335647 +.00000000 +00000-0 +71561-3 0 00002
2 68616 97.2849 344.9999 0001616 90.6952 195.3870 15.49166580 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001616 |
| inclination: | 97.2849° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 344.9999° |
| argument of perigee: | 90.6952° |
| revolutions per day: | 15.49166580 |
| mean anomaly at epoch: | 195.3870° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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