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 66944U 26145.61901515 +.00000000 +00000-0 +76949-3 0 00006
2 66944 53.1598 0.5084 0001924 109.7970 250.3240 15.34412990 02
| Epoch (UTC): | 25 May 2026 14:51:22 |
| Eccentricity: | 0.0001924 |
| inclination: | 53.1598° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 0.5084° |
| argument of perigee: | 109.7970° |
| revolutions per day: | 15.34412990 |
| mean anomaly at epoch: | 250.3240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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