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 58550U 26145.47184375 +.00000000 +00000-0 +11687-3 0 00009
2 58550 53.1611 65.9130 0001111 89.6229 270.4900 15.30209198 06
| Epoch (UTC): | 25 May 2026 11:19:27 |
| Eccentricity: | 0.0001111 |
| inclination: | 53.1611° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 65.9130° |
| argument of perigee: | 89.6229° |
| revolutions per day: | 15.30209198 |
| mean anomaly at epoch: | 270.4900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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