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 26162.52940336 +.00000000 +00000-0 +80461-4 0 00003
2 07434 74.0463 303.5080 0019504 124.3189 235.9815 14.38235938 09
| Epoch (UTC): | 11 June 2026 12:42:20 |
| Eccentricity: | 0.0019504 |
| inclination: | 74.0463° |
| perigee height: | 750 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 303.5080° |
| argument of perigee: | 124.3189° |
| revolutions per day: | 14.38235938 |
| mean anomaly at epoch: | 235.9815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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