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 60118U 26145.35241245 +.00000000 +00000-0 -25702-6 0 00006
2 60118 53.1591 203.3727 0001085 76.1422 283.9717 15.69704161 09
| Epoch (UTC): | 25 May 2026 08:27:28 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 203.3727° |
| argument of perigee: | 76.1422° |
| revolutions per day: | 15.69704161 |
| mean anomaly at epoch: | 283.9717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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