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 47932U 26145.61713442 +.00000000 +00000-0 +26776-3 0 00005
2 47932 97.3926 41.3236 0006020 26.7559 333.3986 15.20184089 07
| Epoch (UTC): | 25 May 2026 14:48:40 |
| Eccentricity: | 0.0006020 |
| inclination: | 97.3926° |
| perigee height: | 501 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 41.3236° |
| argument of perigee: | 26.7559° |
| revolutions per day: | 15.20184089 |
| mean anomaly at epoch: | 333.3986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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