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 15543U 26145.99447551 +.00000000 +00000-0 +00000-0 0 00003
2 15543 12.6949 313.7568 0132235 55.9352 118.4554 0.99807159 05
| Epoch (UTC): | 25 May 2026 23:52:02 |
| Eccentricity: | 0.0132235 |
| inclination: | 12.6949° |
| perigee height: | 35358 km |
| apogee height: | 36477 km |
| right ascension of ascending node: | 313.7568° |
| argument of perigee: | 55.9352° |
| revolutions per day: | 0.99807159 |
| mean anomaly at epoch: | 118.4554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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