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 62590U 26145.01636944 +.00000000 +00000-0 +14758-2 0 00003
2 62590 43.0036 25.6255 0002387 258.5596 101.5004 15.70894325 00
| Epoch (UTC): | 25 May 2026 00:23:34 |
| Eccentricity: | 0.0002387 |
| inclination: | 43.0036° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 25.6255° |
| argument of perigee: | 258.5596° |
| revolutions per day: | 15.70894325 |
| mean anomaly at epoch: | 101.5004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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