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 67524U 26145.51323818 +.00000000 +00000-0 +73500-4 0 00005
2 67524 50.0093 77.0741 0000914 28.1592 331.9330 13.29329658 00
| Epoch (UTC): | 25 May 2026 12:19:03 |
| Eccentricity: | 0.0000914 |
| inclination: | 50.0093° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 77.0741° |
| argument of perigee: | 28.1592° |
| revolutions per day: | 13.29329658 |
| mean anomaly at epoch: | 331.9330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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