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 65815U 25219A 25341.30284067 .00000215 00000-0 12186-3 0 9998
2 65815 98.6577 281.0115 0000615 79.8095 280.3151 14.19902374 10154
| Epoch (UTC): | 07 December 2025 07:16:05 |
| Eccentricity: | 0.0000615 |
| inclination: | 98.6577° |
| perigee height: | 825 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 281.0115° |
| argument of perigee: | 79.8095° |
| revolutions per day: | 14.19902374 |
| mean anomaly at epoch: | 280.3151° |
| orbit number at epoch: | 1015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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