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 68219U 26145.39091538 +.00000000 +00000-0 +70890-3 0 00002
2 68219 97.2867 20.8503 0002192 89.4567 270.6927 15.33446772 03
| Epoch (UTC): | 25 May 2026 09:22:55 |
| Eccentricity: | 0.0002192 |
| inclination: | 97.2867° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8503° |
| argument of perigee: | 89.4567° |
| revolutions per day: | 15.33446772 |
| mean anomaly at epoch: | 270.6927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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