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 51852U 26145.42621679 +.00000000 +00000-0 +33859-3 0 00000
2 51852 53.2141 34.6351 0001508 99.1588 260.9575 15.08813128 06
| Epoch (UTC): | 25 May 2026 10:13:45 |
| Eccentricity: | 0.0001508 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 34.6351° |
| argument of perigee: | 99.1588° |
| revolutions per day: | 15.08813128 |
| mean anomaly at epoch: | 260.9575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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