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 26088.16154852 +.00000000 +00000-0 +11689-3 0 00008
2 15483 74.0452 225.3159 0017661 137.5023 34.3406 14.37797051 08
| Epoch (UTC): | 29 March 2026 03:52:37 |
| Eccentricity: | 0.0017661 |
| inclination: | 74.0452° |
| perigee height: | 753 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 225.3159° |
| argument of perigee: | 137.5023° |
| revolutions per day: | 14.37797051 |
| mean anomaly at epoch: | 34.3406° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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