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 47699U 26145.45021245 +.00000000 +00000-0 +68338-4 0 00001
2 47699 98.4318 218.4226 0001761 263.2649 96.8340 14.40806349 01
| Epoch (UTC): | 25 May 2026 10:48:18 |
| Eccentricity: | 0.0001761 |
| inclination: | 98.4318° |
| perigee height: | 755 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 218.4226° |
| argument of perigee: | 263.2649° |
| revolutions per day: | 14.40806349 |
| mean anomaly at epoch: | 96.8340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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