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 55743U 26145.18067559 +.00000000 +00000-0 +89223-4 0 00004
2 55743 70.0008 51.7654 0003013 270.6195 89.4619 14.98323219 05
| Epoch (UTC): | 25 May 2026 04:20:10 |
| Eccentricity: | 0.0003013 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.7654° |
| argument of perigee: | 270.6195° |
| revolutions per day: | 14.98323219 |
| mean anomaly at epoch: | 89.4619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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