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 62770U 26145.20934705 +.00000000 +00000-0 +89024-3 0 00009
2 62770 53.1594 326.5324 0001421 85.8368 274.2796 15.31718858 06
| Epoch (UTC): | 25 May 2026 05:01:27 |
| Eccentricity: | 0.0001421 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 326.5324° |
| argument of perigee: | 85.8368° |
| revolutions per day: | 15.31718858 |
| mean anomaly at epoch: | 274.2796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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