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 60187U 26145.25440800 +.00000000 +00000-0 +13950-4 0 00008
2 60187 53.1591 143.5115 0001156 82.5338 277.5811 15.69705472 07
| Epoch (UTC): | 25 May 2026 06:06:20 |
| Eccentricity: | 0.0001156 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 143.5115° |
| argument of perigee: | 82.5338° |
| revolutions per day: | 15.69705472 |
| mean anomaly at epoch: | 277.5811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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