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 26106.40977632 +.00000000 +00000-0 +34147-4 0 00007
2 27432 98.8762 159.6124 0049031 275.9598 94.0903 14.14554253 09
| Epoch (UTC): | 16 April 2026 09:50:04 |
| Eccentricity: | 0.0049031 |
| inclination: | 98.8762° |
| perigee height: | 808 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 159.6124° |
| argument of perigee: | 275.9598° |
| revolutions per day: | 14.14554253 |
| mean anomaly at epoch: | 94.0903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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