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 62320U 26145.40800066 +.00000000 +00000-0 +35664-3 0 00005
2 62320 53.1579 184.5170 0001122 82.8966 277.2162 15.30208759 03
| Epoch (UTC): | 25 May 2026 09:47:31 |
| Eccentricity: | 0.0001122 |
| inclination: | 53.1579° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.5170° |
| argument of perigee: | 82.8966° |
| revolutions per day: | 15.30208759 |
| mean anomaly at epoch: | 277.2162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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