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 33842U 93036CK 24357.86376897 .00002097 00000-0 64461-3 0 9998
2 33842 74.0322 157.8041 0047981 352.4192 7.6233 14.41523180832217
| Epoch (UTC): | 22 December 2024 20:43:49 |
| Eccentricity: | 0.0047981 |
| inclination: | 74.0322° |
| perigee height: | 719 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 157.8041° |
| argument of perigee: | 352.4192° |
| revolutions per day: | 14.41523180 |
| mean anomaly at epoch: | 7.6233° |
| orbit number at epoch: | 83221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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