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 13114U 26106.91907758 +.00000000 +00000-0 +29529-4 0 00005
2 13114 82.5405 155.8515 0015960 89.8870 83.4954 13.84788552 01
| Epoch (UTC): | 16 April 2026 22:03:28 |
| Eccentricity: | 0.0015960 |
| inclination: | 82.5405° |
| perigee height: | 935 km |
| apogee height: | 959 km |
| right ascension of ascending node: | 155.8515° |
| argument of perigee: | 89.8870° |
| revolutions per day: | 13.84788552 |
| mean anomaly at epoch: | 83.4954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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