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 23266.50821900 .00019541 00000-0 47845-3 0 9990
2 16495 82.4643 283.4752 0010135 62.6001 297.6275 15.40579540 65335
| Epoch (UTC): | 23 September 2023 12:11:50 |
| Eccentricity: | 0.0010135 |
| inclination: | 82.4643° |
| perigee height: | 437 km |
| apogee height: | 451 km |
| right ascension of ascending node: | 283.4752° |
| argument of perigee: | 62.6001° |
| revolutions per day: | 15.40579540 |
| mean anomaly at epoch: | 297.6275° |
| orbit number at epoch: | 6533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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