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 08800U 76032B 24281.34863874 .00000342 00000-0 17764-3 0 9991
2 08800 81.2496 140.2197 0093920 186.4157 173.5820 14.10470814494178
| Epoch (UTC): | 07 October 2024 08:22:02 |
| Eccentricity: | 0.0093920 |
| inclination: | 81.2496° |
| perigee height: | 790 km |
| apogee height: | 926 km |
| right ascension of ascending node: | 140.2197° |
| argument of perigee: | 186.4157° |
| revolutions per day: | 14.10470814 |
| mean anomaly at epoch: | 173.5820° |
| orbit number at epoch: | 49417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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