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 13758U 26039.60308894 +.00000000 +00000-0 +83460-4 0 00000
2 13758 82.9097 102.7060 0028639 117.9530 242.4533 13.79151346 04
| Epoch (UTC): | 08 February 2026 14:28:26 |
| Eccentricity: | 0.0028639 |
| inclination: | 82.9097° |
| perigee height: | 946 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 102.7060° |
| argument of perigee: | 117.9530° |
| revolutions per day: | 13.79151346 |
| mean anomaly at epoch: | 242.4533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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