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 52933U 26145.59235507 +.00000000 +00000-0 +00000-0 0 00009
2 52933 0.0201 287.2817 0001219 130.8924 259.2587 1.00274343 04
| Epoch (UTC): | 25 May 2026 14:12:59 |
| Eccentricity: | 0.0001219 |
| inclination: | 0.0201° |
| perigee height: | 35781 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 287.2817° |
| argument of perigee: | 130.8924° |
| revolutions per day: | 1.00274343 |
| mean anomaly at epoch: | 259.2587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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