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 52793U 26145.53503683 +.00000000 +00000-0 +34574-3 0 00006
2 52793 49.9974 289.5305 0006453 81.8123 278.3554 15.00358245 00
| Epoch (UTC): | 25 May 2026 12:50:27 |
| Eccentricity: | 0.0006453 |
| inclination: | 49.9974° |
| perigee height: | 561 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 289.5305° |
| argument of perigee: | 81.8123° |
| revolutions per day: | 15.00358245 |
| mean anomaly at epoch: | 278.3554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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