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 60055U 26145.10116179 +.00000000 +00000-0 +35478-4 0 00004
2 60055 53.1610 83.2047 0001424 85.4749 274.6415 15.30192870 01
| Epoch (UTC): | 25 May 2026 02:25:40 |
| Eccentricity: | 0.0001424 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 83.2047° |
| argument of perigee: | 85.4749° |
| revolutions per day: | 15.30192870 |
| mean anomaly at epoch: | 274.6415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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