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 53935U 26145.66668980 +.00000000 +00000-0 +42034-2 0 00000
2 53935 53.2164 287.1102 0001001 40.9199 176.5249 15.68159299 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001001 |
| inclination: | 53.2164° |
| perigee height: | 363 km |
| apogee height: | 365 km |
| right ascension of ascending node: | 287.1102° |
| argument of perigee: | 40.9199° |
| revolutions per day: | 15.68159299 |
| mean anomaly at epoch: | 176.5249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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