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 60532U 26145.62791624 +.00000000 +00000-0 +21062-3 0 00008
2 60532 97.6847 221.0444 0002781 96.0099 264.1439 14.94842472 01
| Epoch (UTC): | 25 May 2026 15:04:11 |
| Eccentricity: | 0.0002781 |
| inclination: | 97.6847° |
| perigee height: | 581 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 221.0444° |
| argument of perigee: | 96.0099° |
| revolutions per day: | 14.94842472 |
| mean anomaly at epoch: | 264.1439° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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