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 62932U 26145.61564785 +.00000000 +00000-0 +18514-3 0 00007
2 62932 98.1311 200.9526 0003532 224.1586 135.9340 14.73313322 06
| Epoch (UTC): | 25 May 2026 14:46:31 |
| Eccentricity: | 0.0003532 |
| inclination: | 98.1311° |
| perigee height: | 648 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 200.9526° |
| argument of perigee: | 224.1586° |
| revolutions per day: | 14.73313322 |
| mean anomaly at epoch: | 135.9340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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