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 27688U 99057MU 25200.39136639 .00001339 00000-0 33194-3 0 9999
2 27688 98.5420 255.7203 0082646 181.6480 193.9454 14.51591397217571
| Epoch (UTC): | 19 July 2025 09:23:34 |
| Eccentricity: | 0.0082646 |
| inclination: | 98.5420° |
| perigee height: | 662 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 255.7203° |
| argument of perigee: | 181.6480° |
| revolutions per day: | 14.51591397 |
| mean anomaly at epoch: | 193.9454° |
| orbit number at epoch: | 21757 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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