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 23087.26561876 .00032550 00000-0 51148-3 0 9993
2 41465 97.0107 320.1745 0008105 161.5471 333.1986 15.53539026387388
| Epoch (UTC): | 28 March 2023 06:22:29 |
| Eccentricity: | 0.0008105 |
| inclination: | 97.0107° |
| perigee height: | 401 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 320.1745° |
| argument of perigee: | 161.5471° |
| revolutions per day: | 15.53539026 |
| mean anomaly at epoch: | 333.1986° |
| orbit number at epoch: | 38738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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