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 15338U 26088.17849000 +.00000000 +00000-0 +17556-3 0 00003
2 15338 66.5689 114.0123 0013753 338.0485 22.0015 14.19279130 01
| Epoch (UTC): | 29 March 2026 04:17:01 |
| Eccentricity: | 0.0013753 |
| inclination: | 66.5689° |
| perigee height: | 818 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 114.0123° |
| argument of perigee: | 338.0485° |
| revolutions per day: | 14.19279130 |
| mean anomaly at epoch: | 22.0015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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