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 16987U 86074B 24287.88134559 .00001419 00000-0 16503-3 0 9995
2 16987 82.5151 323.3706 0019321 83.0153 89.5429 14.84511028 34003
| Epoch (UTC): | 13 October 2024 21:09:08 |
| Eccentricity: | 0.0019321 |
| inclination: | 82.5151° |
| perigee height: | 601 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 323.3706° |
| argument of perigee: | 83.0153° |
| revolutions per day: | 14.84511028 |
| mean anomaly at epoch: | 89.5429° |
| orbit number at epoch: | 3400 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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