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 47806U 26145.53345723 +.00000000 +00000-0 +67730-4 0 00005
2 47806 53.1561 245.5076 0002027 88.8888 271.2345 15.30198492 02
| Epoch (UTC): | 25 May 2026 12:48:10 |
| Eccentricity: | 0.0002027 |
| inclination: | 53.1561° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 245.5076° |
| argument of perigee: | 88.8888° |
| revolutions per day: | 15.30198492 |
| mean anomaly at epoch: | 271.2345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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