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 60156U 26145.48633744 +.00000000 +00000-0 +75222-5 0 00001
2 60156 53.1607 323.2406 0001267 88.0698 272.0448 15.30188832 03
| Epoch (UTC): | 25 May 2026 11:40:19 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.2406° |
| argument of perigee: | 88.0698° |
| revolutions per day: | 15.30188832 |
| mean anomaly at epoch: | 272.0448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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