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 47391U 26145.42181069 +.00000000 +00000-0 +75844-3 0 00007
2 47391 53.0679 45.8442 0002369 100.2186 259.9072 15.10980872 06
| Epoch (UTC): | 25 May 2026 10:07:24 |
| Eccentricity: | 0.0002369 |
| inclination: | 53.0679° |
| perigee height: | 532 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 45.8442° |
| argument of perigee: | 100.2186° |
| revolutions per day: | 15.10980872 |
| mean anomaly at epoch: | 259.9072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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