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 61182U 26144.28427986 +.00000000 +00000-0 +00000-0 0 00004
2 61182 55.1908 221.9692 0005630 222.4383 196.4466 1.70474466 02
| Epoch (UTC): | 24 May 2026 06:49:21 |
| Eccentricity: | 0.0005630 |
| inclination: | 55.1908° |
| perigee height: | 23205 km |
| apogee height: | 23239 km |
| right ascension of ascending node: | 221.9692° |
| argument of perigee: | 222.4383° |
| revolutions per day: | 1.70474466 |
| mean anomaly at epoch: | 196.4466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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