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 58024U 26145.11778707 +.00000000 +00000-0 +20492-3 0 00008
2 58024 97.5777 226.9884 0003697 128.8063 231.3502 15.20344292 03
| Epoch (UTC): | 25 May 2026 02:49:36 |
| Eccentricity: | 0.0003697 |
| inclination: | 97.5777° |
| perigee height: | 502 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 226.9884° |
| argument of perigee: | 128.8063° |
| revolutions per day: | 15.20344292 |
| mean anomaly at epoch: | 231.3502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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