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 16615U 86019C 24276.95147841 .00001518 00000-0 57230-3 0 9998
2 16615 98.2688 308.7844 0012920 79.5062 347.1666 14.32715760 20763
| Epoch (UTC): | 02 October 2024 22:50:07 |
| Eccentricity: | 0.0012920 |
| inclination: | 98.2688° |
| perigee height: | 773 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 308.7844° |
| argument of perigee: | 79.5062° |
| revolutions per day: | 14.32715760 |
| mean anomaly at epoch: | 347.1666° |
| orbit number at epoch: | 2076 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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