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 53916U 26145.47998801 +.00000000 +00000-0 +22486-4 0 00007
2 53916 53.2137 309.0469 0001483 90.5238 269.5924 15.08835687 09
| Epoch (UTC): | 25 May 2026 11:31:10 |
| Eccentricity: | 0.0001483 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.0469° |
| argument of perigee: | 90.5238° |
| revolutions per day: | 15.08835687 |
| mean anomaly at epoch: | 269.5924° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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