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 52846U 26145.43132309 +.00000000 +00000-0 +54941-3 0 00007
2 52846 53.2118 49.6231 0001580 99.1528 260.9643 15.08788484 03
| Epoch (UTC): | 25 May 2026 10:21:06 |
| Eccentricity: | 0.0001580 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.6231° |
| argument of perigee: | 99.1528° |
| revolutions per day: | 15.08788484 |
| mean anomaly at epoch: | 260.9643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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