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 57085U 26145.37915303 +.00000000 +00000-0 -37800-4 0 00000
2 57085 43.0063 22.6280 0001392 251.5507 108.5194 15.27576575 01
| Epoch (UTC): | 25 May 2026 09:05:58 |
| Eccentricity: | 0.0001392 |
| inclination: | 43.0063° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 22.6280° |
| argument of perigee: | 251.5507° |
| revolutions per day: | 15.27576575 |
| mean anomaly at epoch: | 108.5194° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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