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 39676U 87060AP 24279.54015367 .00002053 00000-0 78311-3 0 9990
2 39676 65.0104 312.5822 0021784 264.2990 95.5611 14.32990230547765
| Epoch (UTC): | 05 October 2024 12:57:49 |
| Eccentricity: | 0.0021784 |
| inclination: | 65.0104° |
| perigee height: | 766 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 312.5822° |
| argument of perigee: | 264.2990° |
| revolutions per day: | 14.32990230 |
| mean anomaly at epoch: | 95.5611° |
| orbit number at epoch: | 54776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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