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 is defined by the following mean orbital elements,
1 15483U 26065.51907427 +.00000000 +00000-0 +87052-4 0 00004
2 15483 74.0432 266.9833 0018572 185.5554 195.1557 14.37779856 06
| Epoch (UTC): | 06 March 2026 12:27:28 |
| Eccentricity: | 0.0018572 |
| inclination: | 74.0432° |
| perigee height: | 753 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 266.9833° |
| argument of perigee: | 185.5554° |
| revolutions per day: | 14.37779856 |
| mean anomaly at epoch: | 195.1557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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