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 53715U 26145.36958059 +.00000000 +00000-0 +21659-3 0 00003
2 53715 53.2175 269.6087 0001511 128.4393 231.6735 15.08854038 01
| Epoch (UTC): | 25 May 2026 08:52:11 |
| Eccentricity: | 0.0001511 |
| inclination: | 53.2175° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 269.6087° |
| argument of perigee: | 128.4393° |
| revolutions per day: | 15.08854038 |
| mean anomaly at epoch: | 231.6735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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