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 53630U 26145.52423255 +.00000000 +00000-0 +74806-4 0 00005
2 53630 53.2152 239.2689 0001133 89.3309 270.7813 15.08839247 01
| Epoch (UTC): | 25 May 2026 12:34:53 |
| Eccentricity: | 0.0001133 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.2689° |
| argument of perigee: | 89.3309° |
| revolutions per day: | 15.08839247 |
| mean anomaly at epoch: | 270.7813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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