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 52853U 26145.50003470 +.00000000 +00000-0 +34417-2 0 00004
2 52853 53.2183 39.1820 0002148 106.2517 131.1630 15.12518351 04
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0002148 |
| inclination: | 53.2183° |
| perigee height: | 527 km |
| apogee height: | 530 km |
| right ascension of ascending node: | 39.1820° |
| argument of perigee: | 106.2517° |
| revolutions per day: | 15.12518351 |
| mean anomaly at epoch: | 131.1630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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