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 50478U 26145.09320102 +.00000000 +00000-0 -66377-3 0 00005
2 50478 87.8918 25.6514 0001595 90.0009 270.1302 13.11418632 03
| Epoch (UTC): | 25 May 2026 02:14:12 |
| Eccentricity: | 0.0001595 |
| inclination: | 87.8918° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6514° |
| argument of perigee: | 90.0009° |
| revolutions per day: | 13.11418632 |
| mean anomaly at epoch: | 270.1302° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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