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 58558U 26145.61234292 +.00000000 +00000-0 +21347-3 0 00001
2 58558 34.9917 221.9949 0009356 118.4567 241.7090 15.17428977 01
| Epoch (UTC): | 25 May 2026 14:41:46 |
| Eccentricity: | 0.0009356 |
| inclination: | 34.9917° |
| perigee height: | 507 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 221.9949° |
| argument of perigee: | 118.4567° |
| revolutions per day: | 15.17428977 |
| mean anomaly at epoch: | 241.7090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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