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 47655U 26145.50917205 +.00000000 +00000-0 +12976-3 0 00005
2 47655 53.1599 67.7570 0001401 85.1994 274.9168 15.31703413 00
| Epoch (UTC): | 25 May 2026 12:13:12 |
| Eccentricity: | 0.0001401 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 67.7570° |
| argument of perigee: | 85.1994° |
| revolutions per day: | 15.31703413 |
| mean anomaly at epoch: | 274.9168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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