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 19046U 88032B 24281.51633872 .00015307 00000-0 88548-3 0 9995
2 19046 97.4619 260.4180 0028916 229.2676 130.6044 15.11989176973868
| Epoch (UTC): | 07 October 2024 12:23:31 |
| Eccentricity: | 0.0028916 |
| inclination: | 97.4619° |
| perigee height: | 510 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 260.4180° |
| argument of perigee: | 229.2676° |
| revolutions per day: | 15.11989176 |
| mean anomaly at epoch: | 130.6044° |
| orbit number at epoch: | 97386 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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