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 26138.18087955 +.00000000 +00000-0 +34228-4 0 00007
2 27432 98.8720 191.1923 0050117 184.3733 246.7192 14.14559107 01
| Epoch (UTC): | 18 May 2026 04:20:27 |
| Eccentricity: | 0.0050117 |
| inclination: | 98.8720° |
| perigee height: | 808 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 191.1923° |
| argument of perigee: | 184.3733° |
| revolutions per day: | 14.14559107 |
| mean anomaly at epoch: | 246.7192° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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