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 58526U 26145.43737545 +.00000000 +00000-0 +11945-2 0 00007
2 58526 43.0013 44.9269 0006366 203.0859 156.9700 15.08777827 01
| Epoch (UTC): | 25 May 2026 10:29:49 |
| Eccentricity: | 0.0006366 |
| inclination: | 43.0013° |
| perigee height: | 536 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 44.9269° |
| argument of perigee: | 203.0859° |
| revolutions per day: | 15.08777827 |
| mean anomaly at epoch: | 156.9700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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