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 26053.56137948 +.00000000 +00000-0 +66134-4 0 00000
2 14973 82.9405 337.2763 0030939 231.9420 307.4328 13.75610427 03
| Epoch (UTC): | 22 February 2026 13:28:23 |
| Eccentricity: | 0.0030939 |
| inclination: | 82.9405° |
| perigee height: | 957 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 337.2763° |
| argument of perigee: | 231.9420° |
| revolutions per day: | 13.75610427 |
| mean anomaly at epoch: | 307.4328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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