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 07574U 26088.21282292 +.00000000 +00000-0 +33297-4 0 00006
2 07574 81.2354 37.5893 0016356 169.5049 190.6468 14.12051268 02
| Epoch (UTC): | 29 March 2026 05:06:27 |
| Eccentricity: | 0.0016356 |
| inclination: | 81.2354° |
| perigee height: | 841 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 37.5893° |
| argument of perigee: | 169.5049° |
| revolutions per day: | 14.12051268 |
| mean anomaly at epoch: | 190.6468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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