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 41465U 16026B 23337.12181558 .00059487 00000-0 45662-3 0 9993
2 41465 96.9647 206.4911 0004121 348.5479 11.5691 15.71889192426369
| Epoch (UTC): | 03 December 2023 02:55:24 |
| Eccentricity: | 0.0004121 |
| inclination: | 96.9647° |
| perigee height: | 351 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 206.4911° |
| argument of perigee: | 348.5479° |
| revolutions per day: | 15.71889192 |
| mean anomaly at epoch: | 11.5691° |
| orbit number at epoch: | 42636 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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