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 07714U 26069.85585823 +.00000000 +00000-0 +31429-4 0 00002
2 07714 81.1952 325.5418 0028148 268.0622 91.7324 14.08463177 01
| Epoch (UTC): | 10 March 2026 20:32:26 |
| Eccentricity: | 0.0028148 |
| inclination: | 81.1952° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 325.5418° |
| argument of perigee: | 268.0622° |
| revolutions per day: | 14.08463177 |
| mean anomaly at epoch: | 91.7324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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