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 08162U 26105.41844781 +.00000000 +00000-0 +44045-2 0 00000
2 08162 100.8446 339.3372 0156477 327.1049 207.7237 12.50665590 05
| Epoch (UTC): | 15 April 2026 10:02:33 |
| Eccentricity: | 0.0156477 |
| inclination: | 100.8446° |
| perigee height: | 1339 km |
| apogee height: | 1584 km |
| right ascension of ascending node: | 339.3372° |
| argument of perigee: | 327.1049° |
| revolutions per day: | 12.50665590 |
| mean anomaly at epoch: | 207.7237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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