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 57079U 26145.06378951 +.00000000 +00000-0 +57339-4 0 00009
2 57079 43.0064 24.5650 0001365 268.3672 91.7023 15.27581871 05
| Epoch (UTC): | 25 May 2026 01:31:51 |
| Eccentricity: | 0.0001365 |
| inclination: | 43.0064° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 24.5650° |
| argument of perigee: | 268.3672° |
| revolutions per day: | 15.27581871 |
| mean anomaly at epoch: | 91.7023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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