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 60192U 26145.42099253 +.00000000 +00000-0 +78759-5 0 00004
2 60192 53.1592 143.1390 0001085 80.6572 279.4569 15.69700728 05
| Epoch (UTC): | 25 May 2026 10:06:13 |
| Eccentricity: | 0.0001085 |
| inclination: | 53.1592° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 143.1390° |
| argument of perigee: | 80.6572° |
| revolutions per day: | 15.69700728 |
| mean anomaly at epoch: | 279.4569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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