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 61692U 26145.61322383 +.00000000 +00000-0 +48526-4 0 00002
2 61692 53.1578 7.1790 0000701 89.8248 270.2850 15.69709252 06
| Epoch (UTC): | 25 May 2026 14:43:02 |
| Eccentricity: | 0.0000701 |
| inclination: | 53.1578° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 7.1790° |
| argument of perigee: | 89.8248° |
| revolutions per day: | 15.69709252 |
| mean anomaly at epoch: | 270.2850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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