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 53246U 26145.60238667 +.00000000 +00000-0 -58255-5 0 00000
2 53246 53.2146 218.8475 0001122 89.0800 271.0321 15.08840362 02
| Epoch (UTC): | 25 May 2026 14:27:26 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 218.8475° |
| argument of perigee: | 89.0800° |
| revolutions per day: | 15.08840362 |
| mean anomaly at epoch: | 271.0321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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