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 43107U 26144.72427791 +.00000000 +00000-0 +00000-0 0 00004
2 43107 54.3496 303.1323 0005245 88.6329 271.4059 1.86227819 07
| Epoch (UTC): | 24 May 2026 17:22:57 |
| Eccentricity: | 0.0005245 |
| inclination: | 54.3496° |
| perigee height: | 21514 km |
| apogee height: | 21543 km |
| right ascension of ascending node: | 303.1323° |
| argument of perigee: | 88.6329° |
| revolutions per day: | 1.86227819 |
| mean anomaly at epoch: | 271.4059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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