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 57052U 26145.04658692 +.00000000 +00000-0 +30391-4 0 00000
2 57052 43.0060 39.1500 0001509 256.4175 103.6508 15.27575812 03
| Epoch (UTC): | 25 May 2026 01:07:05 |
| Eccentricity: | 0.0001509 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 39.1500° |
| argument of perigee: | 256.4175° |
| revolutions per day: | 15.27575812 |
| mean anomaly at epoch: | 103.6508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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