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 52986U 26145.61619749 +.00000000 +00000-0 +40528-3 0 00006
2 52986 53.2144 108.7815 0001379 94.2358 265.8792 15.08809570 04
| Epoch (UTC): | 25 May 2026 14:47:19 |
| Eccentricity: | 0.0001379 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 108.7815° |
| argument of perigee: | 94.2358° |
| revolutions per day: | 15.08809570 |
| mean anomaly at epoch: | 265.8792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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