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 61784U 26145.62368234 +.00000000 +00000-0 +64818-3 0 00001
2 61784 97.2987 21.0116 0008748 20.5558 339.6047 15.55441285 05
| Epoch (UTC): | 25 May 2026 14:58:06 |
| Eccentricity: | 0.0008748 |
| inclination: | 97.2987° |
| perigee height: | 395 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 21.0116° |
| argument of perigee: | 20.5558° |
| revolutions per day: | 15.55441285 |
| mean anomaly at epoch: | 339.6047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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