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 26067.59878816 +.00000000 +00000-0 +48101-4 0 00002
2 27432 98.8841 121.0110 0050533 27.3021 92.5486 14.14547474 00
| Epoch (UTC): | 08 March 2026 14:22:15 |
| Eccentricity: | 0.0050533 |
| inclination: | 98.8841° |
| perigee height: | 807 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 121.0110° |
| argument of perigee: | 27.3021° |
| revolutions per day: | 14.14547474 |
| mean anomaly at epoch: | 92.5486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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