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 66962U 26145.46145647 +.00000000 +00000-0 +67772-3 0 00009
2 66962 43.0010 310.3192 0001600 259.5466 100.5206 15.27591142 03
| Epoch (UTC): | 25 May 2026 11:04:29 |
| Eccentricity: | 0.0001600 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 310.3192° |
| argument of perigee: | 259.5466° |
| revolutions per day: | 15.27591142 |
| mean anomaly at epoch: | 100.5206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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