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 13718U 26088.19831331 +.00000000 +00000-0 +56487-4 0 00000
2 13718 81.2482 65.8312 0053021 188.0840 171.9486 14.15936171 06
| Epoch (UTC): | 29 March 2026 04:45:34 |
| Eccentricity: | 0.0053021 |
| inclination: | 81.2482° |
| perigee height: | 801 km |
| apogee height: | 877 km |
| right ascension of ascending node: | 65.8312° |
| argument of perigee: | 188.0840° |
| revolutions per day: | 14.15936171 |
| mean anomaly at epoch: | 171.9486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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