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 57919U 26145.62118818 +.00000000 +00000-0 -70573-6 0 00006
2 57919 43.0018 250.7463 0001277 290.3161 69.7553 15.27585408 05
| Epoch (UTC): | 25 May 2026 14:54:30 |
| Eccentricity: | 0.0001277 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.7463° |
| argument of perigee: | 290.3161° |
| revolutions per day: | 15.27585408 |
| mean anomaly at epoch: | 69.7553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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