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 33841U 93036CJ 24357.68453543 .00001017 00000-0 35014-3 0 9994
2 33841 74.0363 211.4131 0020328 20.3459 41.9562 14.37125069830124
| Epoch (UTC): | 22 December 2024 16:25:43 |
| Eccentricity: | 0.0020328 |
| inclination: | 74.0363° |
| perigee height: | 753 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 211.4131° |
| argument of perigee: | 20.3459° |
| revolutions per day: | 14.37125069 |
| mean anomaly at epoch: | 41.9562° |
| orbit number at epoch: | 83012 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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