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 52650U 26145.36826054 +.00000000 +00000-0 +51702-4 0 00002
2 52650 53.2140 265.0032 0001326 83.1474 276.9669 15.08838516 02
| Epoch (UTC): | 25 May 2026 08:50:17 |
| Eccentricity: | 0.0001326 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 265.0032° |
| argument of perigee: | 83.1474° |
| revolutions per day: | 15.08838516 |
| mean anomaly at epoch: | 276.9669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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