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 26040.25603425 +.00000000 +00000-0 +80957-4 0 00009
2 13758 82.9095 102.2166 0028658 116.1952 244.2159 13.79151487 04
| Epoch (UTC): | 09 February 2026 06:08:41 |
| Eccentricity: | 0.0028658 |
| inclination: | 82.9095° |
| perigee height: | 946 km |
| apogee height: | 988 km |
| right ascension of ascending node: | 102.2166° |
| argument of perigee: | 116.1952° |
| revolutions per day: | 13.79151487 |
| mean anomaly at epoch: | 244.2159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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