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 47321U 26145.52857178 +.00000000 +00000-0 +00000-0 0 00001
2 47321 1.7746 337.9907 0003277 87.7328 89.1905 1.00269922 09
| Epoch (UTC): | 25 May 2026 12:41:08 |
| Eccentricity: | 0.0003277 |
| inclination: | 1.7746° |
| perigee height: | 35773 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 337.9907° |
| argument of perigee: | 87.7328° |
| revolutions per day: | 1.00269922 |
| mean anomaly at epoch: | 89.1905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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