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 61753U 26145.61860463 +.00000000 +00000-0 +55111-3 0 00003
2 61753 97.3014 21.0347 0006791 26.5717 333.5883 15.53226335 04
| Epoch (UTC): | 25 May 2026 14:50:47 |
| Eccentricity: | 0.0006791 |
| inclination: | 97.3014° |
| perigee height: | 403 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 21.0347° |
| argument of perigee: | 26.5717° |
| revolutions per day: | 15.53226335 |
| mean anomaly at epoch: | 333.5883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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