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 47936U 26145.63303737 +.00000000 +00000-0 +14213-3 0 00006
2 47936 97.5430 29.7728 0012823 33.2305 326.9721 14.98640361 08
| Epoch (UTC): | 25 May 2026 15:11:34 |
| Eccentricity: | 0.0012823 |
| inclination: | 97.5430° |
| perigee height: | 562 km |
| apogee height: | 580 km |
| right ascension of ascending node: | 29.7728° |
| argument of perigee: | 33.2305° |
| revolutions per day: | 14.98640361 |
| mean anomaly at epoch: | 326.9721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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