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 43833U 26145.59327669 +.00000000 +00000-0 +18084-3 0 00003
2 43833 97.3186 210.6409 0009625 207.6004 152.4726 15.28046560 04
| Epoch (UTC): | 25 May 2026 14:14:19 |
| Eccentricity: | 0.0009625 |
| inclination: | 97.3186° |
| perigee height: | 475 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 210.6409° |
| argument of perigee: | 207.6004° |
| revolutions per day: | 15.28046560 |
| mean anomaly at epoch: | 152.4726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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