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 53535U 26145.10282733 +.00000000 +00000-0 +60504-4 0 00007
2 53535 53.2155 91.0853 0001410 80.2804 279.8348 15.08840589 07
| Epoch (UTC): | 25 May 2026 02:28:04 |
| Eccentricity: | 0.0001410 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 91.0853° |
| argument of perigee: | 80.2804° |
| revolutions per day: | 15.08840589 |
| mean anomaly at epoch: | 279.8348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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