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 23705U 95058B 24357.52294371 -.00000221 00000-0 -89117-4 0 9995
2 23705 71.0220 28.5220 0010187 69.1854 291.0359 14.15409141505289
| Epoch (UTC): | 22 December 2024 12:33:02 |
| Eccentricity: | 0.0010187 |
| inclination: | 71.0220° |
| perigee height: | 833 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 28.5220° |
| argument of perigee: | 69.1854° |
| revolutions per day: | 14.15409141 |
| mean anomaly at epoch: | 291.0359° |
| orbit number at epoch: | 50528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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