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 34874U 93036ACM 22176.90032853 .00000757 00000-0 30992-3 0 9990
2 34874 74.0400 220.3984 0060082 196.2973 339.6088 14.27919090689309
| Epoch (UTC): | 25 June 2022 21:36:28 |
| Eccentricity: | 0.0060082 |
| inclination: | 74.0400° |
| perigee height: | 755 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 220.3984° |
| argument of perigee: | 196.2973° |
| revolutions per day: | 14.27919090 |
| mean anomaly at epoch: | 339.6088° |
| orbit number at epoch: | 68930 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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