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 51986U 26145.45748118 +.00000000 +00000-0 +49870-3 0 00009
2 51986 53.2132 54.3424 0001437 100.2583 259.8571 15.08801329 07
| Epoch (UTC): | 25 May 2026 10:58:46 |
| Eccentricity: | 0.0001437 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 54.3424° |
| argument of perigee: | 100.2583° |
| revolutions per day: | 15.08801329 |
| mean anomaly at epoch: | 259.8571° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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