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 26076.20693012 +.00000000 +00000-0 +94263-4 0 00003
2 07434 74.0436 102.4577 0021527 301.2968 58.6078 14.38192697 00
| Epoch (UTC): | 17 March 2026 04:57:58 |
| Eccentricity: | 0.0021527 |
| inclination: | 74.0436° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 102.4577° |
| argument of perigee: | 301.2968° |
| revolutions per day: | 14.38192697 |
| mean anomaly at epoch: | 58.6078° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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