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 66923U 26145.17942221 +.00000000 +00000-0 +56697-4 0 00002
2 66923 50.0089 228.2133 0001086 211.6427 148.4380 13.29323782 07
| Epoch (UTC): | 25 May 2026 04:18:22 |
| Eccentricity: | 0.0001086 |
| inclination: | 50.0089° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 228.2133° |
| argument of perigee: | 211.6427° |
| revolutions per day: | 13.29323782 |
| mean anomaly at epoch: | 148.4380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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