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 59537U 26145.37791213 +.00000000 +00000-0 +46622-3 0 00006
2 59537 42.9974 270.3579 0000677 279.2271 80.8504 15.27605925 06
| Epoch (UTC): | 25 May 2026 09:04:11 |
| Eccentricity: | 0.0000677 |
| inclination: | 42.9974° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 270.3579° |
| argument of perigee: | 279.2271° |
| revolutions per day: | 15.27605925 |
| mean anomaly at epoch: | 80.8504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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