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 52833U 26145.14330341 +.00000000 +00000-0 -13429-3 0 00004
2 52833 53.2148 50.9036 0001528 74.9229 285.1932 15.08851822 08
| Epoch (UTC): | 25 May 2026 03:26:21 |
| Eccentricity: | 0.0001528 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 50.9036° |
| argument of perigee: | 74.9229° |
| revolutions per day: | 15.08851822 |
| mean anomaly at epoch: | 285.1932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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