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 26064.24263522 +.00000000 +00000-0 +12038-3 0 00002
2 07434 74.0452 124.4885 0021107 325.3463 34.6315 14.38184879 06
| Epoch (UTC): | 05 March 2026 05:49:23 |
| Eccentricity: | 0.0021107 |
| inclination: | 74.0452° |
| perigee height: | 749 km |
| apogee height: | 780 km |
| right ascension of ascending node: | 124.4885° |
| argument of perigee: | 325.3463° |
| revolutions per day: | 14.38184879 |
| mean anomaly at epoch: | 34.6315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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