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 68620U 26145.58335647 +.00000000 +00000-0 -23771-1 0 00006
2 68620 97.2841 345.1711 0001431 99.3152 226.2381 15.62622065 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001431 |
| inclination: | 97.2841° |
| perigee height: | 379 km |
| apogee height: | 381 km |
| right ascension of ascending node: | 345.1711° |
| argument of perigee: | 99.3152° |
| revolutions per day: | 15.62622065 |
| mean anomaly at epoch: | 226.2381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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