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 26075.16353458 +.00000000 +00000-0 +10017-3 0 00008
2 07434 74.0436 104.3791 0021501 303.3827 56.5270 14.38192139 00
| Epoch (UTC): | 16 March 2026 03:55:29 |
| Eccentricity: | 0.0021501 |
| inclination: | 74.0436° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 104.3791° |
| argument of perigee: | 303.3827° |
| revolutions per day: | 14.38192139 |
| mean anomaly at epoch: | 56.5270° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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