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 33914U 93036DT 22184.02231450 .00000343 00000-0 29781-3 0 9995
2 33914 74.0898 285.3410 0313623 319.1398 217.5372 13.69547183668759
| Epoch (UTC): | 03 July 2022 00:32:07 |
| Eccentricity: | 0.0313623 |
| inclination: | 74.0898° |
| perigee height: | 770 km |
| apogee height: | 1232 km |
| right ascension of ascending node: | 285.3410° |
| argument of perigee: | 319.1398° |
| revolutions per day: | 13.69547183 |
| mean anomaly at epoch: | 217.5372° |
| orbit number at epoch: | 66875 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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