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 13354U 26042.27724503 +.00000000 +00000-0 +56553-4 0 00001
2 13354 82.9628 149.2375 0050545 248.9922 110.5826 13.79253876 03
| Epoch (UTC): | 11 February 2026 06:39:13 |
| Eccentricity: | 0.0050545 |
| inclination: | 82.9628° |
| perigee height: | 929 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 149.2375° |
| argument of perigee: | 248.9922° |
| revolutions per day: | 13.79253876 |
| mean anomaly at epoch: | 110.5826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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