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 13149U 26109.22664747 +.00000000 +00000-0 +51053-4 0 00005
2 13149 74.0393 92.8150 0013986 229.1124 130.8818 14.36705951 09
| Epoch (UTC): | 19 April 2026 05:26:22 |
| Eccentricity: | 0.0013986 |
| inclination: | 74.0393° |
| perigee height: | 759 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 92.8150° |
| argument of perigee: | 229.1124° |
| revolutions per day: | 14.36705951 |
| mean anomaly at epoch: | 130.8818° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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