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 67333U 26145.03144779 +.00000000 +00000-0 +35352-3 0 00009
2 67333 43.0023 254.1795 0002126 279.1476 80.9135 15.27586798 00
| Epoch (UTC): | 25 May 2026 00:45:17 |
| Eccentricity: | 0.0002126 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.1795° |
| argument of perigee: | 279.1476° |
| revolutions per day: | 15.27586798 |
| mean anomaly at epoch: | 80.9135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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