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 26067.44053771 +.00000000 +00000-0 +52842-4 0 00009
2 07714 81.1956 327.8997 0027955 275.0393 84.7586 14.08462931 09
| Epoch (UTC): | 08 March 2026 10:34:22 |
| Eccentricity: | 0.0027955 |
| inclination: | 81.1956° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 327.8997° |
| argument of perigee: | 275.0393° |
| revolutions per day: | 14.08462931 |
| mean anomaly at epoch: | 84.7586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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