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 62014U 26144.90674499 +.00000000 +00000-0 +11533-2 0 00006
2 62014 53.1573 25.7090 0000992 38.0035 322.1053 15.69727158 08
| Epoch (UTC): | 24 May 2026 21:45:42 |
| Eccentricity: | 0.0000992 |
| inclination: | 53.1573° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 25.7090° |
| argument of perigee: | 38.0035° |
| revolutions per day: | 15.69727158 |
| mean anomaly at epoch: | 322.1053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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