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 23087.90772899 .00029293 00000-0 46019-3 0 9994
2 41465 97.0104 320.8003 0008184 159.0932 324.4127 15.53564368387488
| Epoch (UTC): | 28 March 2023 21:47:07 |
| Eccentricity: | 0.0008184 |
| inclination: | 97.0104° |
| perigee height: | 401 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 320.8003° |
| argument of perigee: | 159.0932° |
| revolutions per day: | 15.53564368 |
| mean anomaly at epoch: | 324.4127° |
| orbit number at epoch: | 38748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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