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 26103.70939366 +.00000000 +00000-0 +33054-4 0 00008
2 07734 114.9908 103.5877 0019848 304.0233 55.8960 14.19173793 09
| Epoch (UTC): | 13 April 2026 17:01:31 |
| Eccentricity: | 0.0019848 |
| inclination: | 114.9908° |
| perigee height: | 814 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 103.5877° |
| argument of perigee: | 304.0233° |
| revolutions per day: | 14.19173793 |
| mean anomaly at epoch: | 55.8960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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