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 14973U 26106.63598287 +.00000000 +00000-0 +53976-4 0 00004
2 14973 82.9328 297.8817 0033487 85.2872 342.3727 13.75616319 07
| Epoch (UTC): | 16 April 2026 15:15:48 |
| Eccentricity: | 0.0033487 |
| inclination: | 82.9328° |
| perigee height: | 955 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 297.8817° |
| argument of perigee: | 85.2872° |
| revolutions per day: | 13.75616319 |
| mean anomaly at epoch: | 342.3727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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