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 15370U 84111B 24282.23078683 .00005339 00000-0 61890-3 0 9993
2 15370 82.5195 23.2026 0019125 243.2968 116.6290 14.85173138160143
| Epoch (UTC): | 08 October 2024 05:32:19 |
| Eccentricity: | 0.0019125 |
| inclination: | 82.5195° |
| perigee height: | 599 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 23.2026° |
| argument of perigee: | 243.2968° |
| revolutions per day: | 14.85173138 |
| mean anomaly at epoch: | 116.6290° |
| orbit number at epoch: | 16014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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