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 20805U 90083B 24276.90311948 .00000174 00000-0 16222-3 0 9999
2 20805 82.9343 242.1725 0031411 147.0657 231.8593 13.76124081709841
| Epoch (UTC): | 02 October 2024 21:40:29 |
| Eccentricity: | 0.0031411 |
| inclination: | 82.9343° |
| perigee height: | 954 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 242.1725° |
| argument of perigee: | 147.0657° |
| revolutions per day: | 13.76124081 |
| mean anomaly at epoch: | 231.8593° |
| orbit number at epoch: | 70984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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