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 68622U 26145.58335647 +.00000000 +00000-0 -30889-1 0 00006
2 68622 97.2844 345.0989 0001944 75.6874 79.9785 15.55873779 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001944 |
| inclination: | 97.2844° |
| perigee height: | 398 km |
| apogee height: | 401 km |
| right ascension of ascending node: | 345.0989° |
| argument of perigee: | 75.6874° |
| revolutions per day: | 15.55873779 |
| mean anomaly at epoch: | 79.9785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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