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 33722U 99025DHK 24279.29009866 .00010568 00000-0 44374-2 0 9990
2 33722 98.6028 299.9034 0164330 66.8804 294.9596 14.19012819860203
| Epoch (UTC): | 05 October 2024 06:57:44 |
| Eccentricity: | 0.0164330 |
| inclination: | 98.6028° |
| perigee height: | 710 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 299.9034° |
| argument of perigee: | 66.8804° |
| revolutions per day: | 14.19012819 |
| mean anomaly at epoch: | 294.9596° |
| orbit number at epoch: | 86020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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