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 20301U 88102J 24358.21239331 .00000149 00000-0 10273-3 0 9991
2 20301 70.9974 78.8940 0017920 253.5193 106.3960 14.14370693829111
| Epoch (UTC): | 23 December 2024 05:05:50 |
| Eccentricity: | 0.0017920 |
| inclination: | 70.9974° |
| perigee height: | 831 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 78.8940° |
| argument of perigee: | 253.5193° |
| revolutions per day: | 14.14370693 |
| mean anomaly at epoch: | 106.3960° |
| orbit number at epoch: | 82911 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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