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 26065.66456685 +.00000000 +00000-0 +53448-4 0 00005
2 07714 81.1958 329.6333 0027862 280.2048 79.5980 14.08462579 05
| Epoch (UTC): | 06 March 2026 15:56:58 |
| Eccentricity: | 0.0027862 |
| inclination: | 81.1958° |
| perigee height: | 844 km |
| apogee height: | 885 km |
| right ascension of ascending node: | 329.6333° |
| argument of perigee: | 280.2048° |
| revolutions per day: | 14.08462579 |
| mean anomaly at epoch: | 79.5980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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