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 47086U 26087.84099036 +.00000000 +00000-0 +10785-2 0 00003
2 47086 82.5507 305.0955 0011404 246.5745 113.4238 14.22359199 01
| Epoch (UTC): | 28 March 2026 20:11:01 |
| Eccentricity: | 0.0011404 |
| inclination: | 82.5507° |
| perigee height: | 809 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 305.0955° |
| argument of perigee: | 246.5745° |
| revolutions per day: | 14.22359199 |
| mean anomaly at epoch: | 113.4238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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