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 53847U 26145.46897969 +.00000000 +00000-0 -35060-4 0 00005
2 53847 53.2151 309.3758 0001465 101.0543 259.0614 15.08846071 08
| Epoch (UTC): | 25 May 2026 11:15:19 |
| Eccentricity: | 0.0001465 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.3758° |
| argument of perigee: | 101.0543° |
| revolutions per day: | 15.08846071 |
| mean anomaly at epoch: | 259.0614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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