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 20465U 90010A 24280.72642489 .00013305 00000-0 92679-3 0 9993
2 20465 82.4904 195.9140 0011198 290.3925 69.6098 15.05291108863990
| Epoch (UTC): | 06 October 2024 17:26:03 |
| Eccentricity: | 0.0011198 |
| inclination: | 82.4904° |
| perigee height: | 543 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 195.9140° |
| argument of perigee: | 290.3925° |
| revolutions per day: | 15.05291108 |
| mean anomaly at epoch: | 69.6098° |
| orbit number at epoch: | 86399 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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