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 23152.45854038 -.00000009 00000-0 -24474-4 0 9994
2 16728 82.9539 164.3292 0029575 235.4751 233.9193 13.76830118859622
| Epoch (UTC): | 01 June 2023 11:00:17 |
| Eccentricity: | 0.0029575 |
| inclination: | 82.9539° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 164.3292° |
| argument of perigee: | 235.4751° |
| revolutions per day: | 13.76830118 |
| mean anomaly at epoch: | 233.9193° |
| orbit number at epoch: | 85962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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