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 60155U 26145.66668980 +.00000000 +00000-0 -53859-3 0 00001
2 60155 53.1605 322.3683 0001363 92.7891 198.8222 15.30202588 01
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001363 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 322.3683° |
| argument of perigee: | 92.7891° |
| revolutions per day: | 15.30202588 |
| mean anomaly at epoch: | 198.8222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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