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 26106.47815691 +.00000000 +00000-0 +83676-4 0 00000
2 15362 90.1158 81.9312 0031226 349.2246 126.5828 13.23062752 04
| Epoch (UTC): | 16 April 2026 11:28:32 |
| Eccentricity: | 0.0031226 |
| inclination: | 90.1158° |
| perigee height: | 1149 km |
| apogee height: | 1197 km |
| right ascension of ascending node: | 81.9312° |
| argument of perigee: | 349.2246° |
| revolutions per day: | 13.23062752 |
| mean anomaly at epoch: | 126.5828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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