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 60150U 26145.47050352 +.00000000 +00000-0 +84811-4 0 00005
2 60150 53.1605 323.1419 0000858 84.9517 275.1581 15.30178041 01
| Epoch (UTC): | 25 May 2026 11:17:31 |
| Eccentricity: | 0.0000858 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 323.1419° |
| argument of perigee: | 84.9517° |
| revolutions per day: | 15.30178041 |
| mean anomaly at epoch: | 275.1581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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