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 57253U 26145.14130257 +.00000000 +00000-0 +13824-4 0 00008
2 57253 43.0015 308.0069 0001325 273.9660 86.1040 15.27579840 04
| Epoch (UTC): | 25 May 2026 03:23:28 |
| Eccentricity: | 0.0001325 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 308.0069° |
| argument of perigee: | 273.9660° |
| revolutions per day: | 15.27579840 |
| mean anomaly at epoch: | 86.1040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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