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 51850U 26108.76630939 +.00000000 +00000-0 +00000-0 0 00002
2 51850 0.0085 60.4621 0000434 35.5189 249.7860 1.00273320 09
| Epoch (UTC): | 18 April 2026 18:23:29 |
| Eccentricity: | 0.0000434 |
| inclination: | 0.0085° |
| perigee height: | 35784 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 60.4621° |
| argument of perigee: | 35.5189° |
| revolutions per day: | 1.00273320 |
| mean anomaly at epoch: | 249.7860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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