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 30775U 07006D 23312.51377346 .64784629 19388-5 33254-3 0 9992
2 30775 35.4153 66.1965 0006514 150.0013 306.1704 16.54751544926071
| Epoch (UTC): | 08 November 2023 12:19:50 |
| Eccentricity: | 0.0006514 |
| inclination: | 35.4153° |
| perigee height: | 122 km |
| apogee height: | 131 km |
| right ascension of ascending node: | 66.1965° |
| argument of perigee: | 150.0013° |
| revolutions per day: | 16.54751544 |
| mean anomaly at epoch: | 306.1704° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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