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 36292U 08056H 24282.57050696 .00009642 00000-0 55673-2 0 9996
2 36292 98.7129 41.3182 0158665 152.2345 208.7405 14.03063273813267
| Epoch (UTC): | 08 October 2024 13:41:31 |
| Eccentricity: | 0.0158665 |
| inclination: | 98.7129° |
| perigee height: | 768 km |
| apogee height: | 998 km |
| right ascension of ascending node: | 41.3182° |
| argument of perigee: | 152.2345° |
| revolutions per day: | 14.03063273 |
| mean anomaly at epoch: | 208.7405° |
| orbit number at epoch: | 81326 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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