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 25637U 99008D 24284.58515681 .00002144 00000-0 51445-3 0 9991
2 25637 96.4557 312.8611 0140525 53.8612 58.7981 14.48236073351763
| Epoch (UTC): | 10 October 2024 14:02:37 |
| Eccentricity: | 0.0140525 |
| inclination: | 96.4557° |
| perigee height: | 631 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 312.8611° |
| argument of perigee: | 53.8612° |
| revolutions per day: | 14.48236073 |
| mean anomaly at epoch: | 58.7981° |
| orbit number at epoch: | 35176 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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