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 62929U 26145.56927995 +.00000000 +00000-0 +15561-3 0 00002
2 62929 98.0958 199.9776 0001568 8.4699 351.6535 14.73297915 09
| Epoch (UTC): | 25 May 2026 13:39:45 |
| Eccentricity: | 0.0001568 |
| inclination: | 98.0958° |
| perigee height: | 649 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 199.9776° |
| argument of perigee: | 8.4699° |
| revolutions per day: | 14.73297915 |
| mean anomaly at epoch: | 351.6535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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