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 26071.13455735 +.00000000 +00000-0 +35982-4 0 00002
2 07714 81.1951 324.2935 0028248 264.3556 95.4393 14.08463450 07
| Epoch (UTC): | 12 March 2026 03:13:45 |
| Eccentricity: | 0.0028248 |
| inclination: | 81.1951° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 324.2935° |
| argument of perigee: | 264.3556° |
| revolutions per day: | 14.08463450 |
| mean anomaly at epoch: | 95.4393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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