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 52756U 26145.39794051 +.00000000 +00000-0 +32284-3 0 00006
2 52756 97.6578 301.9643 0005879 142.5204 217.6458 15.50456448 07
| Epoch (UTC): | 25 May 2026 09:33:02 |
| Eccentricity: | 0.0005879 |
| inclination: | 97.6578° |
| perigee height: | 411 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 301.9643° |
| argument of perigee: | 142.5204° |
| revolutions per day: | 15.50456448 |
| mean anomaly at epoch: | 217.6458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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