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 8923U 76061A 24358.13501592 .00000330 00000-0 12782-3 0 9999
2 8923 74.0527 244.2274 0019065 256.7792 103.1233 14.33826467532932
| Epoch (UTC): | 23 December 2024 03:14:25 |
| Eccentricity: | 0.0019065 |
| inclination: | 74.0527° |
| perigee height: | 765 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 244.2274° |
| argument of perigee: | 256.7792° |
| revolutions per day: | 14.33826467 |
| mean anomaly at epoch: | 103.1233° |
| orbit number at epoch: | 53293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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