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 61186U 26143.76045272 +.00000000 +00000-0 +00000-0 0 00004
2 61186 54.4958 303.0900 0002982 311.8334 49.3076 1.86230046 07
| Epoch (UTC): | 23 May 2026 18:15:03 |
| Eccentricity: | 0.0002982 |
| inclination: | 54.4958° |
| perigee height: | 21520 km |
| apogee height: | 21536 km |
| right ascension of ascending node: | 303.0900° |
| argument of perigee: | 311.8334° |
| revolutions per day: | 1.86230046 |
| mean anomaly at epoch: | 49.3076° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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