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 24251.87873594 .00003490 00000-0 11904-2 0 9998
2 33841 74.0389 45.9177 0021552 243.5055 273.9090 14.36673666814926
| Epoch (UTC): | 07 September 2024 21:05:22 |
| Eccentricity: | 0.0021552 |
| inclination: | 74.0389° |
| perigee height: | 754 km |
| apogee height: | 785 km |
| right ascension of ascending node: | 45.9177° |
| argument of perigee: | 243.5055° |
| revolutions per day: | 14.36673666 |
| mean anomaly at epoch: | 273.9090° |
| orbit number at epoch: | 81492 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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