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 59616U 26145.20571609 +.00000000 +00000-0 +35471-4 0 00002
2 59616 43.0061 325.8824 0000646 280.8531 79.2248 15.27579987 00
| Epoch (UTC): | 25 May 2026 04:56:13 |
| Eccentricity: | 0.0000646 |
| inclination: | 43.0061° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 325.8824° |
| argument of perigee: | 280.8531° |
| revolutions per day: | 15.27579987 |
| mean anomaly at epoch: | 79.2248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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