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 58862U 26145.45505772 +.00000000 +00000-0 +43374-4 0 00000
2 58862 43.0015 175.3085 0001196 279.7596 80.3120 15.27581371 09
| Epoch (UTC): | 25 May 2026 10:55:16 |
| Eccentricity: | 0.0001196 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.3085° |
| argument of perigee: | 279.7596° |
| revolutions per day: | 15.27581371 |
| mean anomaly at epoch: | 80.3120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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