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 53734U 26144.74035573 +.00000000 +00000-0 +50923-4 0 00009
2 53734 53.2151 272.7883 0001146 88.8379 271.2745 15.08840448 03
| Epoch (UTC): | 24 May 2026 17:46:06 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 272.7883° |
| argument of perigee: | 88.8379° |
| revolutions per day: | 15.08840448 |
| mean anomaly at epoch: | 271.2745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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