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 16495U 86006A 19338.73820992 +.00000692 +00000-0 +26554-4 0 9992
2 16495 082.4743 247.0334 0011115 277.5837 082.4138 15.24708633853232
| Epoch (UTC): | 04 December 2019 17:43:01 |
| Eccentricity: | 0.0011115 |
| inclination: | 82.4743° |
| perigee height: | 484 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 247.0334° |
| argument of perigee: | 277.5837° |
| revolutions per day: | 15.24708633 |
| mean anomaly at epoch: | 82.4138° |
| orbit number at epoch: | 85323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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