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 16728U 86037B 24276.23040478 .00000283 00000-0 27091-3 0 9992
2 16728 82.9573 161.7301 0029872 310.8094 167.8535 13.76952997926888
| Epoch (UTC): | 02 October 2024 05:31:46 |
| Eccentricity: | 0.0029872 |
| inclination: | 82.9573° |
| perigee height: | 953 km |
| apogee height: | 996 km |
| right ascension of ascending node: | 161.7301° |
| argument of perigee: | 310.8094° |
| revolutions per day: | 13.76952997 |
| mean anomaly at epoch: | 167.8535° |
| orbit number at epoch: | 92688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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