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 47227U 26145.62792887 +.00000000 +00000-0 +20849-3 0 00008
2 47227 82.5035 316.4631 0020213 227.9336 132.0025 12.42892955 01
| Epoch (UTC): | 25 May 2026 15:04:13 |
| Eccentricity: | 0.0020213 |
| inclination: | 82.5035° |
| perigee height: | 1478 km |
| apogee height: | 1510 km |
| right ascension of ascending node: | 316.4631° |
| argument of perigee: | 227.9336° |
| revolutions per day: | 12.42892955 |
| mean anomaly at epoch: | 132.0025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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