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 53286U 26145.54163005 +.00000000 +00000-0 -56479-4 0 00005
2 53286 53.2113 198.8101 0001219 77.8480 282.2649 15.08843667 07
| Epoch (UTC): | 25 May 2026 12:59:56 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.2113° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 198.8101° |
| argument of perigee: | 77.8480° |
| revolutions per day: | 15.08843667 |
| mean anomaly at epoch: | 282.2649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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