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 53652U 26145.37487027 +.00000000 +00000-0 +52853-4 0 00007
2 53652 97.4460 25.3073 0001839 73.6125 286.5304 15.05664488 03
| Epoch (UTC): | 25 May 2026 08:59:48 |
| Eccentricity: | 0.0001839 |
| inclination: | 97.4460° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 25.3073° |
| argument of perigee: | 73.6125° |
| revolutions per day: | 15.05664488 |
| mean anomaly at epoch: | 286.5304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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