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 57479U 26134.61903050 +.00000000 +00000-0 +00000-0 0 00005
2 57479 0.0118 316.7243 0001102 107.6557 295.6476 1.00271791 02
| Epoch (UTC): | 14 May 2026 14:51:24 |
| Eccentricity: | 0.0001102 |
| inclination: | 0.0118° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 316.7243° |
| argument of perigee: | 107.6557° |
| revolutions per day: | 1.00271791 |
| mean anomaly at epoch: | 295.6476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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