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 68720U 26145.58335647 +.00000000 +00000-0 +16495-2 0 00002
2 68720 53.1597 37.0606 0001190 101.5923 260.9400 15.49245487 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.1597° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 37.0606° |
| argument of perigee: | 101.5923° |
| revolutions per day: | 15.49245487 |
| mean anomaly at epoch: | 260.9400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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