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 27783U 26113.23244837 +.00000000 +00000-0 +73320-4 0 00005
2 27783 28.9963 113.6382 0003206 276.2491 83.7733 14.65999330 02
| Epoch (UTC): | 23 April 2026 05:34:43 |
| Eccentricity: | 0.0003206 |
| inclination: | 28.9963° |
| perigee height: | 672 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 113.6382° |
| argument of perigee: | 276.2491° |
| revolutions per day: | 14.65999330 |
| mean anomaly at epoch: | 83.7733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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