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 62332U 26145.57553490 +.00000000 +00000-0 +73691-4 0 00005
2 62332 86.5032 351.0405 0001389 81.9136 278.2156 13.24408164 03
| Epoch (UTC): | 25 May 2026 13:48:46 |
| Eccentricity: | 0.0001389 |
| inclination: | 86.5032° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 351.0405° |
| argument of perigee: | 81.9136° |
| revolutions per day: | 13.24408164 |
| mean anomaly at epoch: | 278.2156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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