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 52621U 26145.37377257 +.00000000 +00000-0 +15130-4 0 00002
2 52621 53.2144 284.8711 0001294 89.2378 270.8762 15.08834807 07
| Epoch (UTC): | 25 May 2026 08:58:13 |
| Eccentricity: | 0.0001294 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.8711° |
| argument of perigee: | 89.2378° |
| revolutions per day: | 15.08834807 |
| mean anomaly at epoch: | 270.8762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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