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 55610U 26145.37143620 +.00000000 +00000-0 +12830-6 0 00004
2 55610 43.0054 281.4335 0001678 274.6957 85.3703 15.27577158 07
| Epoch (UTC): | 25 May 2026 08:54:52 |
| Eccentricity: | 0.0001678 |
| inclination: | 43.0054° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 281.4335° |
| argument of perigee: | 274.6957° |
| revolutions per day: | 15.27577158 |
| mean anomaly at epoch: | 85.3703° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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