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 47719U 26144.06756793 +.00000000 +00000-0 +00000-0 0 00001
2 47719 63.2351 61.1234 7279642 269.8294 14.7586 2.00630669 07
| Epoch (UTC): | 24 May 2026 01:37:17 |
| Eccentricity: | 0.7279642 |
| inclination: | 63.2351° |
| perigee height: | 846 km |
| apogee height: | 39507 km |
| right ascension of ascending node: | 61.1234° |
| argument of perigee: | 269.8294° |
| revolutions per day: | 2.00630669 |
| mean anomaly at epoch: | 14.7586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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