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 14365U 26150.25572479 +.00000000 +00000-0 +00000-0 0 00007
2 14365 13.6259 342.1229 0004589 95.3054 93.1577 1.00204616 04
| Epoch (UTC): | 30 May 2026 06:08:14 |
| Eccentricity: | 0.0004589 |
| inclination: | 13.6259° |
| perigee height: | 35786 km |
| apogee height: | 35825 km |
| right ascension of ascending node: | 342.1229° |
| argument of perigee: | 95.3054° |
| revolutions per day: | 1.00204616 |
| mean anomaly at epoch: | 93.1577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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