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 51752U 26145.19807910 +.00000000 +00000-0 +18746-4 0 00006
2 51752 53.2137 325.5939 0001362 95.2283 264.8865 15.08834556 04
| Epoch (UTC): | 25 May 2026 04:45:14 |
| Eccentricity: | 0.0001362 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 325.5939° |
| argument of perigee: | 95.2283° |
| revolutions per day: | 15.08834556 |
| mean anomaly at epoch: | 264.8865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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