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 53634U 26145.24359419 +.00000000 +00000-0 +16241-3 0 00006
2 53634 53.2158 240.3632 0001144 89.9101 270.2022 15.08837782 09
| Epoch (UTC): | 25 May 2026 05:50:46 |
| Eccentricity: | 0.0001144 |
| inclination: | 53.2158° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 240.3632° |
| argument of perigee: | 89.9101° |
| revolutions per day: | 15.08837782 |
| mean anomaly at epoch: | 270.2022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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