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 10674U 26104.15314580 +.00000000 +00000-0 +88284-5 0 00006
2 10674 69.3657 20.3796 0163961 175.0407 350.8297 13.43712152 06
| Epoch (UTC): | 14 April 2026 03:40:31 |
| Eccentricity: | 0.0163961 |
| inclination: | 69.3657° |
| perigee height: | 973 km |
| apogee height: | 1218 km |
| right ascension of ascending node: | 20.3796° |
| argument of perigee: | 175.0407° |
| revolutions per day: | 13.43712152 |
| mean anomaly at epoch: | 350.8297° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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