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 61119U 24140PM 24357.67112363 .00042538 00000-0 81502-2 0 9999
2 61119 89.0587 335.7022 0098908 322.8365 36.6027 14.60461893 18243
| Epoch (UTC): | 22 December 2024 16:06:25 |
| Eccentricity: | 0.0098908 |
| inclination: | 89.0587° |
| perigee height: | 622 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 335.7022° |
| argument of perigee: | 322.8365° |
| revolutions per day: | 14.60461893 |
| mean anomaly at epoch: | 36.6027° |
| orbit number at epoch: | 1824 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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