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 58075U 26145.29555499 +.00000000 +00000-0 +36161-3 0 00004
2 58075 43.0032 5.0962 0001459 274.7350 85.3335 15.27586957 00
| Epoch (UTC): | 25 May 2026 07:05:35 |
| Eccentricity: | 0.0001459 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.0962° |
| argument of perigee: | 274.7350° |
| revolutions per day: | 15.27586957 |
| mean anomaly at epoch: | 85.3335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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