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 35462U 93036ALG 24356.91267682 .00005360 00000-0 21679-2 0 9993
2 35462 74.0374 193.3185 0090148 314.9939 44.3926 14.25848630613028
| Epoch (UTC): | 21 December 2024 21:54:15 |
| Eccentricity: | 0.0090148 |
| inclination: | 74.0374° |
| perigee height: | 741 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 193.3185° |
| argument of perigee: | 314.9939° |
| revolutions per day: | 14.25848630 |
| mean anomaly at epoch: | 44.3926° |
| orbit number at epoch: | 61302 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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