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 26068.48579330 +.00000000 +00000-0 +10706-3 0 00009
2 07434 74.0447 116.6757 0021288 316.7742 43.1740 14.38187771 06
| Epoch (UTC): | 09 March 2026 11:39:32 |
| Eccentricity: | 0.0021288 |
| inclination: | 74.0447° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 116.6757° |
| argument of perigee: | 316.7742° |
| revolutions per day: | 14.38187771 |
| mean anomaly at epoch: | 43.1740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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