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 58858U 26145.53715694 +.00000000 +00000-0 +25181-4 0 00006
2 58858 43.0023 175.0718 0001228 289.8603 70.2117 15.27575326 07
| Epoch (UTC): | 25 May 2026 12:53:30 |
| Eccentricity: | 0.0001228 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 175.0718° |
| argument of perigee: | 289.8603° |
| revolutions per day: | 15.27575326 |
| mean anomaly at epoch: | 70.2117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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