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 data is extracted from the following two-line orbital elements,
1 2016U 66013A 23271.19694953 .00003684 00000-0 10777-2 0 9991
2 2016 34.0900 209.1752 1177594 355.6775 3.4388 12.61724074614297
| Epoch (UTC): | 28 September 2023 04:43:36 |
| Eccentricity: | 0.1177594 |
| inclination: | 34.0900° |
| perigee height: | 498 km |
| apogee height: | 2333 km |
| right ascension of ascending node: | 209.1752° |
| argument of perigee: | 355.6775° |
| revolutions per day: | 12.61724074 |
| mean anomaly at epoch: | 3.4388° |
| orbit number at epoch: | 61429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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