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 10525U 77119D 24358.18848145 .00009970 00000-0 14380-2 0 9992
2 10525 74.0192 78.1888 0009292 257.0555 102.9581 14.76339150484369
| Epoch (UTC): | 23 December 2024 04:31:24 |
| Eccentricity: | 0.0009292 |
| inclination: | 74.0192° |
| perigee height: | 634 km |
| apogee height: | 647 km |
| right ascension of ascending node: | 78.1888° |
| argument of perigee: | 257.0555° |
| revolutions per day: | 14.76339150 |
| mean anomaly at epoch: | 102.9581° |
| orbit number at epoch: | 48436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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