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 07337U 26088.16978784 +.00000000 +00000-0 +26121-3 0 00002
2 07337 82.9403 338.4343 0431774 265.0222 90.1578 14.66969831 04
| Epoch (UTC): | 29 March 2026 04:04:29 |
| Eccentricity: | 0.0431774 |
| inclination: | 82.9403° |
| perigee height: | 366 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 338.4343° |
| argument of perigee: | 265.0222° |
| revolutions per day: | 14.66969831 |
| mean anomaly at epoch: | 90.1578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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