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 65579U 26145.41576218 +.00000000 +00000-0 +13027-3 0 00003
2 65579 81.3082 32.1242 0004583 265.2582 94.8051 13.83264104 09
| Epoch (UTC): | 25 May 2026 09:58:41 |
| Eccentricity: | 0.0004583 |
| inclination: | 81.3082° |
| perigee height: | 949 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 32.1242° |
| argument of perigee: | 265.2582° |
| revolutions per day: | 13.83264104 |
| mean anomaly at epoch: | 94.8051° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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