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 07434U 26066.19031546 +.00000000 +00000-0 +10533-3 0 00005
2 07434 74.0449 120.9024 0021195 321.3956 38.5681 14.38186018 04
| Epoch (UTC): | 07 March 2026 04:34:03 |
| Eccentricity: | 0.0021195 |
| inclination: | 74.0449° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 120.9024° |
| argument of perigee: | 321.3956° |
| revolutions per day: | 14.38186018 |
| mean anomaly at epoch: | 38.5681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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