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 23159.50858572 -.00000001 00000-0 -16207-4 0 9991
2 16728 82.9538 159.1001 0029904 215.0887 258.7414 13.76829916860594
| Epoch (UTC): | 08 June 2023 12:12:21 |
| Eccentricity: | 0.0029904 |
| inclination: | 82.9538° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 159.1001° |
| argument of perigee: | 215.0887° |
| revolutions per day: | 13.76829916 |
| mean anomaly at epoch: | 258.7414° |
| orbit number at epoch: | 86059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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