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 67477U 26108.24989312 +.00000000 +00000-0 +14935-3 0 00004
2 67477 44.9797 348.2073 0010535 46.2987 313.8717 13.99140766 06
| Epoch (UTC): | 18 April 2026 05:59:50 |
| Eccentricity: | 0.0010535 |
| inclination: | 44.9797° |
| perigee height: | 889 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 348.2073° |
| argument of perigee: | 46.2987° |
| revolutions per day: | 13.99140766 |
| mean anomaly at epoch: | 313.8717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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