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 60032U 26145.50511509 +.00000000 +00000-0 +17733-4 0 00003
2 60032 53.1605 78.8906 0001257 87.5430 272.5714 15.30193746 00
| Epoch (UTC): | 25 May 2026 12:07:21 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.8906° |
| argument of perigee: | 87.5430° |
| revolutions per day: | 15.30193746 |
| mean anomaly at epoch: | 272.5714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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