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 50574U 26145.61091948 +.00000000 +00000-0 +00000-0 0 00000
2 50574 0.0764 74.6559 0004306 18.2963 147.3843 1.00268646 01
| Epoch (UTC): | 25 May 2026 14:39:43 |
| Eccentricity: | 0.0004306 |
| inclination: | 0.0764° |
| perigee height: | 35769 km |
| apogee height: | 35806 km |
| right ascension of ascending node: | 74.6559° |
| argument of perigee: | 18.2963° |
| revolutions per day: | 1.00268646 |
| mean anomaly at epoch: | 147.3843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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