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 30633U 99025ANQ 24358.21900478 .00003044 00000-0 18422-2 0 9993
2 30633 98.4531 242.4236 0132105 181.9107 303.5141 14.02894359910685
| Epoch (UTC): | 23 December 2024 05:15:22 |
| Eccentricity: | 0.0132105 |
| inclination: | 98.4531° |
| perigee height: | 788 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 242.4236° |
| argument of perigee: | 181.9107° |
| revolutions per day: | 14.02894359 |
| mean anomaly at epoch: | 303.5141° |
| orbit number at epoch: | 91068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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