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 68562U 26145.03599639 +.00000000 +00000-0 +33394-3 0 00007
2 68562 53.1597 7.2352 0001153 90.9806 269.1329 15.34395624 04
| Epoch (UTC): | 25 May 2026 00:51:50 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 7.2352° |
| argument of perigee: | 90.9806° |
| revolutions per day: | 15.34395624 |
| mean anomaly at epoch: | 269.1329° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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