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 26071.19862795 +.00000000 +00000-0 +10303-3 0 00004
2 07434 74.0442 111.6804 0021391 311.3120 48.6192 14.38189568 02
| Epoch (UTC): | 12 March 2026 04:46:01 |
| Eccentricity: | 0.0021391 |
| inclination: | 74.0442° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 111.6804° |
| argument of perigee: | 311.3120° |
| revolutions per day: | 14.38189568 |
| mean anomaly at epoch: | 48.6192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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