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 08366U 26160.03123610 +.00000000 +00000-0 +00000-0 0 00007
2 08366 4.6269 277.5678 0003513 350.4136 232.1991 1.00262645 01
| Epoch (UTC): | 09 June 2026 00:44:58 |
| Eccentricity: | 0.0003513 |
| inclination: | 4.6269° |
| perigee height: | 35774 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 277.5678° |
| argument of perigee: | 350.4136° |
| revolutions per day: | 1.00262645 |
| mean anomaly at epoch: | 232.1991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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