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 57719U 26145.41243030 +.00000000 +00000-0 +94489-4 0 00005
2 57719 43.0037 44.8359 0001278 274.6632 85.4073 15.27584832 01
| Epoch (UTC): | 25 May 2026 09:53:53 |
| Eccentricity: | 0.0001278 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 44.8359° |
| argument of perigee: | 274.6632° |
| revolutions per day: | 15.27584832 |
| mean anomaly at epoch: | 85.4073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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