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 47997U 26145.19091551 +.00000000 +00000-0 +80792-5 0 00009
2 47997 53.1595 310.9577 0001749 72.7991 287.3201 15.31703204 03
| Epoch (UTC): | 25 May 2026 04:34:55 |
| Eccentricity: | 0.0001749 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 310.9577° |
| argument of perigee: | 72.7991° |
| revolutions per day: | 15.31703204 |
| mean anomaly at epoch: | 287.3201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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