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 52785U 26145.59010002 +.00000000 +00000-0 +24019-3 0 00004
2 52785 49.9945 306.8340 0022676 174.9103 185.2069 14.81288462 06
| Epoch (UTC): | 25 May 2026 14:09:44 |
| Eccentricity: | 0.0022676 |
| inclination: | 49.9945° |
| perigee height: | 609 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 306.8340° |
| argument of perigee: | 174.9103° |
| revolutions per day: | 14.81288462 |
| mean anomaly at epoch: | 185.2069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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