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 47807U 26145.21070637 +.00000000 +00000-0 +21477-4 0 00008
2 47807 53.1568 220.7937 0001319 94.8288 265.2864 15.31709703 08
| Epoch (UTC): | 25 May 2026 05:03:25 |
| Eccentricity: | 0.0001319 |
| inclination: | 53.1568° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 220.7937° |
| argument of perigee: | 94.8288° |
| revolutions per day: | 15.31709703 |
| mean anomaly at epoch: | 265.2864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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