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 43707U 26145.08450286 +.00000000 +00000-0 +00000-0 0 00005
2 43707 54.1682 183.0719 0007646 321.1241 38.8899 1.86226506 06
| Epoch (UTC): | 25 May 2026 02:01:41 |
| Eccentricity: | 0.0007646 |
| inclination: | 54.1682° |
| perigee height: | 21507 km |
| apogee height: | 21550 km |
| right ascension of ascending node: | 183.0719° |
| argument of perigee: | 321.1241° |
| revolutions per day: | 1.86226506 |
| mean anomaly at epoch: | 38.8899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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