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 23339.85892796 .00062272 00000-0 47104-3 0 9997
2 41465 96.9647 209.2252 0003532 337.4057 22.7051 15.72231367426799
| Epoch (UTC): | 05 December 2023 20:36:51 |
| Eccentricity: | 0.0003532 |
| inclination: | 96.9647° |
| perigee height: | 350 km |
| apogee height: | 355 km |
| right ascension of ascending node: | 209.2252° |
| argument of perigee: | 337.4057° |
| revolutions per day: | 15.72231367 |
| mean anomaly at epoch: | 22.7051° |
| orbit number at epoch: | 42679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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