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 58823U 26145.60660095 +.00000000 +00000-0 +69691-3 0 00003
2 58823 97.4322 234.8360 0007593 151.3275 208.8396 15.50687278 04
| Epoch (UTC): | 25 May 2026 14:33:30 |
| Eccentricity: | 0.0007593 |
| inclination: | 97.4322° |
| perigee height: | 410 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 234.8360° |
| argument of perigee: | 151.3275° |
| revolutions per day: | 15.50687278 |
| mean anomaly at epoch: | 208.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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