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 62709U 26145.09114016 +.00000000 +00000-0 +10911-3 0 00002
2 62709 97.7028 223.8994 0001614 153.9641 206.1661 14.94153896 09
| Epoch (UTC): | 25 May 2026 02:11:14 |
| Eccentricity: | 0.0001614 |
| inclination: | 97.7028° |
| perigee height: | 584 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 223.8994° |
| argument of perigee: | 153.9641° |
| revolutions per day: | 14.94153896 |
| mean anomaly at epoch: | 206.1661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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