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 24276.74396104 .00000480 00000-0 27015-3 0 9999
2 23705 71.0220 198.0853 0013423 206.0888 153.9560 14.15380233493858
| Epoch (UTC): | 02 October 2024 17:51:18 |
| Eccentricity: | 0.0013423 |
| inclination: | 71.0220° |
| perigee height: | 831 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 198.0853° |
| argument of perigee: | 206.0888° |
| revolutions per day: | 14.15380233 |
| mean anomaly at epoch: | 153.9560° |
| orbit number at epoch: | 49385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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