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 53979U 26145.53662330 +.00000000 +00000-0 +15297-4 0 00000
2 53979 53.2161 234.1341 0001945 84.2576 275.8638 15.08830844 02
| Epoch (UTC): | 25 May 2026 12:52:44 |
| Eccentricity: | 0.0001945 |
| inclination: | 53.2161° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.1341° |
| argument of perigee: | 84.2576° |
| revolutions per day: | 15.08830844 |
| mean anomaly at epoch: | 275.8638° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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