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 36071U 93036AYJ 23338.61468074 .00014620 00000-0 27683-2 0 9994
2 36071 74.0284 47.7400 0024996 291.1010 68.7486 14.64136131766648
| Epoch (UTC): | 04 December 2023 14:45:08 |
| Eccentricity: | 0.0024996 |
| inclination: | 74.0284° |
| perigee height: | 662 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 47.7400° |
| argument of perigee: | 291.1010° |
| revolutions per day: | 14.64136131 |
| mean anomaly at epoch: | 68.7486° |
| orbit number at epoch: | 76664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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