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 62433U 26145.54544795 +.00000000 +00000-0 +73484-3 0 00001
2 62433 53.1597 338.4351 0001139 82.7286 277.3844 15.30201941 05
| Epoch (UTC): | 25 May 2026 13:05:26 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.4351° |
| argument of perigee: | 82.7286° |
| revolutions per day: | 15.30201941 |
| mean anomaly at epoch: | 277.3844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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