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 23275.07116986 -.00000233 00000-0 -95509-4 0 9993
2 23705 71.0204 247.6490 0011337 24.6242 335.5420 14.15251476442277
| Epoch (UTC): | 02 October 2023 01:42:29 |
| Eccentricity: | 0.0011337 |
| inclination: | 71.0204° |
| perigee height: | 833 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 247.6490° |
| argument of perigee: | 24.6242° |
| revolutions per day: | 14.15251476 |
| mean anomaly at epoch: | 335.5420° |
| orbit number at epoch: | 44227 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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