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 27432U 26156.07555442 +.00000000 +00000-0 +49124-4 0 00007
2 27432 98.8704 208.9736 0050952 133.9745 293.4448 14.14562369 09
| Epoch (UTC): | 05 June 2026 01:48:47 |
| Eccentricity: | 0.0050952 |
| inclination: | 98.8704° |
| perigee height: | 807 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 208.9736° |
| argument of perigee: | 133.9745° |
| revolutions per day: | 14.14562369 |
| mean anomaly at epoch: | 293.4448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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