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 61582U 26145.64999098 +.00000000 +00000-0 -10308-4 0 00004
2 61582 53.1601 277.1663 0001317 316.6523 43.4391 15.69689364 01
| Epoch (UTC): | 25 May 2026 15:35:59 |
| Eccentricity: | 0.0001317 |
| inclination: | 53.1601° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 277.1663° |
| argument of perigee: | 316.6523° |
| revolutions per day: | 15.69689364 |
| mean anomaly at epoch: | 43.4391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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