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 29536U 06015C 25319.84427933 .00024343 00000-0 25001-2 0 9993
2 29536 97.8496 275.4573 0092201 308.0157 51.2760 14.87213457 32144
| Epoch (UTC): | 15 November 2025 20:15:45 |
| Eccentricity: | 0.0092201 |
| inclination: | 97.8496° |
| perigee height: | 542 km |
| apogee height: | 671 km |
| right ascension of ascending node: | 275.4573° |
| argument of perigee: | 308.0157° |
| revolutions per day: | 14.87213457 |
| mean anomaly at epoch: | 51.2760° |
| orbit number at epoch: | 3214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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