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 47361U 26144.99348661 +.00000000 +00000-0 +19245-3 0 00001
2 47361 53.1579 42.2842 0001869 115.6302 244.4892 15.29385241 00
| Epoch (UTC): | 24 May 2026 23:50:37 |
| Eccentricity: | 0.0001869 |
| inclination: | 53.1579° |
| perigee height: | 476 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 42.2842° |
| argument of perigee: | 115.6302° |
| revolutions per day: | 15.29385241 |
| mean anomaly at epoch: | 244.4892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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