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 60879U 24140KJ 24357.46007228 .00001467 00000-0 70948-3 0 9990
2 60879 89.0438 336.3773 0056350 136.8445 223.7181 14.17198565 18163
| Epoch (UTC): | 22 December 2024 11:02:30 |
| Eccentricity: | 0.0056350 |
| inclination: | 89.0438° |
| perigee height: | 794 km |
| apogee height: | 875 km |
| right ascension of ascending node: | 336.3773° |
| argument of perigee: | 136.8445° |
| revolutions per day: | 14.17198565 |
| mean anomaly at epoch: | 223.7181° |
| orbit number at epoch: | 1816 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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