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 58271U 26145.23106563 +.00000000 +00000-0 +55975-3 0 00004
2 58271 97.3826 232.8268 0005355 232.3692 127.7073 15.48134440 07
| Epoch (UTC): | 25 May 2026 05:32:44 |
| Eccentricity: | 0.0005355 |
| inclination: | 97.3826° |
| perigee height: | 419 km |
| apogee height: | 426 km |
| right ascension of ascending node: | 232.8268° |
| argument of perigee: | 232.3692° |
| revolutions per day: | 15.48134440 |
| mean anomaly at epoch: | 127.7073° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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