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 52499U 26145.66668980 +.00000000 +00000-0 +45250-1 0 00006
2 52499 53.2212 61.8185 0001256 71.1474 186.3397 15.36031679 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.2212° |
| perigee height: | 457 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 61.8185° |
| argument of perigee: | 71.1474° |
| revolutions per day: | 15.36031679 |
| mean anomaly at epoch: | 186.3397° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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