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 62884U 26145.23531977 +.00000000 +00000-0 +13879-2 0 00006
2 62884 43.0028 80.2066 0001035 287.3791 72.6963 15.70860435 07
| Epoch (UTC): | 25 May 2026 05:38:51 |
| Eccentricity: | 0.0001035 |
| inclination: | 43.0028° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 80.2066° |
| argument of perigee: | 287.3791° |
| revolutions per day: | 15.70860435 |
| mean anomaly at epoch: | 72.6963° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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