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 52568U 26145.39860464 +.00000000 +00000-0 -92794-4 0 00003
2 52568 53.2129 134.7580 0001142 88.0377 272.0746 15.08849552 04
| Epoch (UTC): | 25 May 2026 09:33:59 |
| Eccentricity: | 0.0001142 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 134.7580° |
| argument of perigee: | 88.0377° |
| revolutions per day: | 15.08849552 |
| mean anomaly at epoch: | 272.0746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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