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 58258U 26145.57466075 +.00000000 +00000-0 +44057-3 0 00002
2 58258 97.3772 231.1448 0005319 238.4061 121.6671 15.47533935 09
| Epoch (UTC): | 25 May 2026 13:47:30 |
| Eccentricity: | 0.0005319 |
| inclination: | 97.3772° |
| perigee height: | 420 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 231.1448° |
| argument of perigee: | 238.4061° |
| revolutions per day: | 15.47533935 |
| mean anomaly at epoch: | 121.6671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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