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 07734U 26106.66906633 +.00000000 +00000-0 +27201-4 0 00004
2 07734 114.9907 111.7117 0020018 303.7048 56.2122 14.19174188 01
| Epoch (UTC): | 16 April 2026 16:03:27 |
| Eccentricity: | 0.0020018 |
| inclination: | 114.9907° |
| perigee height: | 814 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 111.7117° |
| argument of perigee: | 303.7048° |
| revolutions per day: | 14.19174188 |
| mean anomaly at epoch: | 56.2122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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