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 23150.80007612 -.00000004 00000-0 -19226-4 0 9993
2 16728 82.9540 165.5593 0029518 240.3064 293.4057 13.76830252859393
| Epoch (UTC): | 30 May 2023 19:12:06 |
| Eccentricity: | 0.0029518 |
| inclination: | 82.9540° |
| perigee height: | 953 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 165.5593° |
| argument of perigee: | 240.3064° |
| revolutions per day: | 13.76830252 |
| mean anomaly at epoch: | 293.4057° |
| orbit number at epoch: | 85939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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