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 52788U 26145.57541800 +.00000000 +00000-0 +22504-3 0 00007
2 52788 50.0053 307.4472 0009694 63.8777 296.3157 14.81309635 01
| Epoch (UTC): | 25 May 2026 13:48:36 |
| Eccentricity: | 0.0009694 |
| inclination: | 50.0053° |
| perigee height: | 618 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 307.4472° |
| argument of perigee: | 63.8777° |
| revolutions per day: | 14.81309635 |
| mean anomaly at epoch: | 296.3157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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