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 2621U 66111C 24358.49724677 .00001946 00000-0 22776-3 0 9991
2 2621 93.3973 333.9015 0057175 185.8302 174.2264 14.84054522115270
| Epoch (UTC): | 23 December 2024 11:56:02 |
| Eccentricity: | 0.0057175 |
| inclination: | 93.3973° |
| perigee height: | 576 km |
| apogee height: | 656 km |
| right ascension of ascending node: | 333.9015° |
| argument of perigee: | 185.8302° |
| revolutions per day: | 14.84054522 |
| mean anomaly at epoch: | 174.2264° |
| orbit number at epoch: | 11527 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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