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 61470U 24140AAC 24358.37857057 .00150478 00000-0 13813-1 0 9995
2 61470 89.2703 339.1825 0110889 237.0820 121.9705 14.89544954 16330
| Epoch (UTC): | 23 December 2024 09:05:08 |
| Eccentricity: | 0.0110889 |
| inclination: | 89.2703° |
| perigee height: | 522 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 339.1825° |
| argument of perigee: | 237.0820° |
| revolutions per day: | 14.89544954 |
| mean anomaly at epoch: | 121.9705° |
| orbit number at epoch: | 1633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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