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 57057U 26145.11710885 +.00000000 +00000-0 +21761-4 0 00007
2 57057 43.0049 38.7861 0001343 268.4209 91.6489 15.27578640 03
| Epoch (UTC): | 25 May 2026 02:48:38 |
| Eccentricity: | 0.0001343 |
| inclination: | 43.0049° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 38.7861° |
| argument of perigee: | 268.4209° |
| revolutions per day: | 15.27578640 |
| mean anomaly at epoch: | 91.6489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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