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 53257U 26145.58490757 +.00000000 +00000-0 +13973-4 0 00005
2 53257 53.2121 208.9260 0001297 81.6786 278.4353 15.08836137 04
| Epoch (UTC): | 25 May 2026 14:02:16 |
| Eccentricity: | 0.0001297 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 208.9260° |
| argument of perigee: | 81.6786° |
| revolutions per day: | 15.08836137 |
| mean anomaly at epoch: | 278.4353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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