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 47229U 26145.57486941 +.00000000 +00000-0 +57891-5 0 00004
2 47229 82.5017 316.1051 0021127 223.2586 136.6836 12.42891459 05
| Epoch (UTC): | 25 May 2026 13:47:48 |
| Eccentricity: | 0.0021127 |
| inclination: | 82.5017° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 316.1051° |
| argument of perigee: | 223.2586° |
| revolutions per day: | 12.42891459 |
| mean anomaly at epoch: | 136.6836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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