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 52580U 26145.23442610 +.00000000 +00000-0 +20575-4 0 00006
2 52580 53.2136 150.5077 0001190 75.0894 285.0230 15.08836148 05
| Epoch (UTC): | 25 May 2026 05:37:34 |
| Eccentricity: | 0.0001190 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 150.5077° |
| argument of perigee: | 75.0894° |
| revolutions per day: | 15.08836148 |
| mean anomaly at epoch: | 285.0230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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