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 57059U 26145.10811772 +.00000000 +00000-0 +77937-5 0 00002
2 57059 43.0061 38.7366 0001593 267.4389 92.6281 15.27577328 07
| Epoch (UTC): | 25 May 2026 02:35:41 |
| Eccentricity: | 0.0001593 |
| inclination: | 43.0061° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 38.7366° |
| argument of perigee: | 267.4389° |
| revolutions per day: | 15.27577328 |
| mean anomaly at epoch: | 92.6281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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