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 51878C 22022AC 24358.52826389 -.00010489 00000+0 -65764-3 0 3585
2 51878 53.2148 189.5719 0001386 90.5627 24.8194 15.08856288 11
| Epoch (UTC): | 23 December 2024 12:40:42 |
| Eccentricity: | 0.0001386 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 189.5719° |
| argument of perigee: | 90.5627° |
| revolutions per day: | 15.08856288 |
| mean anomaly at epoch: | 24.8194° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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