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 00051U 26106.68571773 +.00000000 +00000-0 -48919-4 0 00004
2 00051 47.2122 239.6644 0107145 14.3648 346.0149 12.18377536 04
| Epoch (UTC): | 16 April 2026 16:27:26 |
| Eccentricity: | 0.0107145 |
| inclination: | 47.2122° |
| perigee height: | 1514 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 239.6644° |
| argument of perigee: | 14.3648° |
| revolutions per day: | 12.18377536 |
| mean anomaly at epoch: | 346.0149° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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