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 15453U 26145.89218252 +.00000000 +00000-0 +00000-0 0 00006
2 15453 11.5289 321.1033 0001963 308.2098 52.5914 0.98856796 02
| Epoch (UTC): | 25 May 2026 21:24:44 |
| Eccentricity: | 0.0001963 |
| inclination: | 11.5289° |
| perigee height: | 36180 km |
| apogee height: | 36196 km |
| right ascension of ascending node: | 321.1033° |
| argument of perigee: | 308.2098° |
| revolutions per day: | 0.98856796 |
| mean anomaly at epoch: | 52.5914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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