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 26102.95997780 +.00000000 +00000-0 +25574-4 0 00004
2 07714 81.1893 293.2113 0030266 175.7034 184.4402 14.08467641 00
| Epoch (UTC): | 12 April 2026 23:02:22 |
| Eccentricity: | 0.0030266 |
| inclination: | 81.1893° |
| perigee height: | 843 km |
| apogee height: | 887 km |
| right ascension of ascending node: | 293.2113° |
| argument of perigee: | 175.7034° |
| revolutions per day: | 14.08467641 |
| mean anomaly at epoch: | 184.4402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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