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 44536U 19060C 24357.85013895 .00032566 00000-0 11059-2 0 9998
2 44536 97.4988 130.0247 0013479 114.5751 245.6895 15.30339417293069
| Epoch (UTC): | 22 December 2024 20:24:12 |
| Eccentricity: | 0.0013479 |
| inclination: | 97.4988° |
| perigee height: | 465 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 130.0247° |
| argument of perigee: | 114.5751° |
| revolutions per day: | 15.30339417 |
| mean anomaly at epoch: | 245.6895° |
| orbit number at epoch: | 29306 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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