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 58980U 26144.86004029 +.00000000 +00000-0 +12455-3 0 00009
2 58980 53.1623 302.9990 0001326 90.8410 269.2743 15.30212324 04
| Epoch (UTC): | 24 May 2026 20:38:27 |
| Eccentricity: | 0.0001326 |
| inclination: | 53.1623° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 302.9990° |
| argument of perigee: | 90.8410° |
| revolutions per day: | 15.30212324 |
| mean anomaly at epoch: | 269.2743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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