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 15362U 26104.18745409 +.00000000 +00000-0 +16993-3 0 00002
2 15362 90.1154 81.9056 0031432 355.5605 15.8867 13.23062344 03
| Epoch (UTC): | 14 April 2026 04:29:56 |
| Eccentricity: | 0.0031432 |
| inclination: | 90.1154° |
| perigee height: | 1149 km |
| apogee height: | 1197 km |
| right ascension of ascending node: | 81.9056° |
| argument of perigee: | 355.5605° |
| revolutions per day: | 13.23062344 |
| mean anomaly at epoch: | 15.8867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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