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 62772U 26145.20010551 +.00000000 +00000-0 +88388-3 0 00007
2 62772 53.1589 327.1817 0001045 69.2053 290.9060 15.31720434 07
| Epoch (UTC): | 25 May 2026 04:48:09 |
| Eccentricity: | 0.0001045 |
| inclination: | 53.1589° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 327.1817° |
| argument of perigee: | 69.2053° |
| revolutions per day: | 15.31720434 |
| mean anomaly at epoch: | 290.9060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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