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 58029U 26145.54048378 +.00000000 +00000-0 +92090-4 0 00008
2 58029 53.1612 81.3144 0001510 75.6749 284.4420 15.30200565 01
| Epoch (UTC): | 25 May 2026 12:58:17 |
| Eccentricity: | 0.0001510 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.3144° |
| argument of perigee: | 75.6749° |
| revolutions per day: | 15.30200565 |
| mean anomaly at epoch: | 284.4420° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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