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 33905U 93036DJ 24357.75061146 .00003098 00000-0 11100-2 0 9997
2 33905 73.8871 252.7130 0060956 213.2315 210.6528 14.33360826825970
| Epoch (UTC): | 22 December 2024 18:00:52 |
| Eccentricity: | 0.0060956 |
| inclination: | 73.8871° |
| perigee height: | 737 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 252.7130° |
| argument of perigee: | 213.2315° |
| revolutions per day: | 14.33360826 |
| mean anomaly at epoch: | 210.6528° |
| orbit number at epoch: | 82597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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