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 16909U 86061B 23088.47253269 -.00000097 00000-0 90379-6 0 9996
2 16909 50.0142 167.9646 0011205 51.0362 44.7880 12.44475028665694
| Epoch (UTC): | 29 March 2023 11:20:26 |
| Eccentricity: | 0.0011205 |
| inclination: | 50.0142° |
| perigee height: | 1479 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 167.9646° |
| argument of perigee: | 51.0362° |
| revolutions per day: | 12.44475028 |
| mean anomaly at epoch: | 44.7880° |
| orbit number at epoch: | 66569 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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