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 36416U 10009D 24277.17328144 .00003667 00000-0 92233-3 0 9996
2 36416 63.3979 292.4448 0644459 359.4436 0.5814 13.71140252729415
| Epoch (UTC): | 03 October 2024 04:09:31 |
| Eccentricity: | 0.0644459 |
| inclination: | 63.3979° |
| perigee height: | 520 km |
| apogee height: | 1470 km |
| right ascension of ascending node: | 292.4448° |
| argument of perigee: | 359.4436° |
| revolutions per day: | 13.71140252 |
| mean anomaly at epoch: | 0.5814° |
| orbit number at epoch: | 72941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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