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 34616U 93036WM 22137.37350247 .00529571 00000-0 14199-1 0 9991
2 34616 74.0072 120.2689 0017246 213.2772 146.7351 15.35627856704011
| Epoch (UTC): | 17 May 2022 08:57:50 |
| Eccentricity: | 0.0017246 |
| inclination: | 74.0072° |
| perigee height: | 447 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 120.2689° |
| argument of perigee: | 213.2772° |
| revolutions per day: | 15.35627856 |
| mean anomaly at epoch: | 146.7351° |
| orbit number at epoch: | 70401 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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