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 53835U 26145.45700448 +.00000000 +00000-0 +94989-4 0 00000
2 53835 53.2133 319.2894 0001208 87.4587 272.6543 15.08837593 07
| Epoch (UTC): | 25 May 2026 10:58:05 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 319.2894° |
| argument of perigee: | 87.4587° |
| revolutions per day: | 15.08837593 |
| mean anomaly at epoch: | 272.6543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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