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 27847U 26106.27705302 +.00000000 +00000-0 +77877-4 0 00002
2 27847 98.6889 115.4842 0008946 351.7042 8.3987 14.23825714 04
| Epoch (UTC): | 16 April 2026 06:38:57 |
| Eccentricity: | 0.0008946 |
| inclination: | 98.6889° |
| perigee height: | 806 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 115.4842° |
| argument of perigee: | 351.7042° |
| revolutions per day: | 14.23825714 |
| mean anomaly at epoch: | 8.3987° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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