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 57958U 26145.62750860 +.00000000 +00000-0 +89305-4 0 00008
2 57958 98.1957 95.3207 0002142 81.0367 279.1075 14.58707814 01
| Epoch (UTC): | 25 May 2026 15:03:36 |
| Eccentricity: | 0.0002142 |
| inclination: | 98.1957° |
| perigee height: | 696 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 95.3207° |
| argument of perigee: | 81.0367° |
| revolutions per day: | 14.58707814 |
| mean anomaly at epoch: | 279.1075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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