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 47397U 26145.61377742 +.00000000 +00000-0 +12609-2 0 00008
2 47397 53.1591 64.9063 0001470 128.5861 231.5273 15.32383069 00
| Epoch (UTC): | 25 May 2026 14:43:50 |
| Eccentricity: | 0.0001470 |
| inclination: | 53.1591° |
| perigee height: | 468 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 64.9063° |
| argument of perigee: | 128.5861° |
| revolutions per day: | 15.32383069 |
| mean anomaly at epoch: | 231.5273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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