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 13272U 82059B 24287.54975614 .00001704 00000-0 19079-3 0 9994
2 13272 82.5091 144.0265 0016490 279.9015 80.0339 14.86249115267848
| Epoch (UTC): | 13 October 2024 13:11:38 |
| Eccentricity: | 0.0016490 |
| inclination: | 82.5091° |
| perigee height: | 598 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 144.0265° |
| argument of perigee: | 279.9015° |
| revolutions per day: | 14.86249115 |
| mean anomaly at epoch: | 80.0339° |
| orbit number at epoch: | 26784 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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