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 45854U 26142.05045963 +.00000000 +00000-0 +00000-0 0 00006
2 45854 56.6536 29.9571 0062928 204.8500 329.5146 2.00559133 06
| Epoch (UTC): | 22 May 2026 01:12:39 |
| Eccentricity: | 0.0062928 |
| inclination: | 56.6536° |
| perigee height: | 20015 km |
| apogee height: | 20350 km |
| right ascension of ascending node: | 29.9571° |
| argument of perigee: | 204.8500° |
| revolutions per day: | 2.00559133 |
| mean anomaly at epoch: | 329.5146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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