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 22331.92871001 .00000278 00000-0 24259-3 0 9992
2 33914 74.0908 42.5075 0312158 41.4189 129.8643 13.69693981688594
| Epoch (UTC): | 27 November 2022 22:17:20 |
| Eccentricity: | 0.0312158 |
| inclination: | 74.0908° |
| perigee height: | 770 km |
| apogee height: | 1231 km |
| right ascension of ascending node: | 42.5075° |
| argument of perigee: | 41.4189° |
| revolutions per day: | 13.69693981 |
| mean anomaly at epoch: | 129.8643° |
| orbit number at epoch: | 68859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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