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 47505U 26145.59250279 +.00000000 +00000-0 +18121-3 0 00007
2 47505 97.2339 191.0209 0004574 289.5631 70.5118 15.34361743 01
| Epoch (UTC): | 25 May 2026 14:13:12 |
| Eccentricity: | 0.0004574 |
| inclination: | 97.2339° |
| perigee height: | 460 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 191.0209° |
| argument of perigee: | 289.5631° |
| revolutions per day: | 15.34361743 |
| mean anomaly at epoch: | 70.5118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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