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 34022U 93036HH 24358.02630817 .00001161 00000-0 38971-3 0 9991
2 34022 74.0525 204.0392 0022377 358.4679 152.3041 14.38202654831158
| Epoch (UTC): | 23 December 2024 00:37:53 |
| Eccentricity: | 0.0022377 |
| inclination: | 74.0525° |
| perigee height: | 748 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 204.0392° |
| argument of perigee: | 358.4679° |
| revolutions per day: | 14.38202654 |
| mean anomaly at epoch: | 152.3041° |
| orbit number at epoch: | 83115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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