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 43476U 18047A 26067.58064799 +.00006523 00000-0 +17716-3 0 07
2 43476 88.9904 211.7667 0013290 135.5614 325.7543 15.37432115434343
| Epoch (UTC): | 08 March 2026 13:56:07 |
| Eccentricity: | 0.0013290 |
| inclination: | 88.9904° |
| perigee height: | 444 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 211.7667° |
| argument of perigee: | 135.5614° |
| revolutions per day: | 15.37432115 |
| mean anomaly at epoch: | 325.7543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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