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 47933U 26145.62577353 +.00000000 +00000-0 +13509-3 0 00006
2 47933 97.5401 29.4802 0015035 43.7874 316.4539 14.98934805 08
| Epoch (UTC): | 25 May 2026 15:01:06 |
| Eccentricity: | 0.0015035 |
| inclination: | 97.5401° |
| perigee height: | 560 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 29.4802° |
| argument of perigee: | 43.7874° |
| revolutions per day: | 14.98934805 |
| mean anomaly at epoch: | 316.4539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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