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 47242U 26145.40435845 +.00000000 +00000-0 +00000-0 0 00003
2 47242 5.3012 76.9914 0083482 278.7830 80.0862 0.95297607 07
| Epoch (UTC): | 25 May 2026 09:42:16 |
| Eccentricity: | 0.0083482 |
| inclination: | 5.3012° |
| perigee height: | 36877 km |
| apogee height: | 37605 km |
| right ascension of ascending node: | 76.9914° |
| argument of perigee: | 278.7830° |
| revolutions per day: | 0.95297607 |
| mean anomaly at epoch: | 80.0862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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