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 60600U 26145.46366213 +.00000000 +00000-0 +30309-4 0 00003
2 60600 53.1623 310.5729 0001211 82.7717 277.3421 15.30194560 08
| Epoch (UTC): | 25 May 2026 11:07:40 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1623° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.5729° |
| argument of perigee: | 82.7717° |
| revolutions per day: | 15.30194560 |
| mean anomaly at epoch: | 277.3421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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