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 23156.52874747 -.00000002 00000-0 -17190-4 0 9995
2 16728 82.9538 161.3103 0029750 223.6781 248.6633 13.76830004860185
| Epoch (UTC): | 05 June 2023 12:41:23 |
| Eccentricity: | 0.0029750 |
| inclination: | 82.9538° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 161.3103° |
| argument of perigee: | 223.6781° |
| revolutions per day: | 13.76830004 |
| mean anomaly at epoch: | 248.6633° |
| orbit number at epoch: | 86018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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