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 47901U 26145.04380388 +.00000000 +00000-0 +11858-2 0 00001
2 47901 53.1568 259.0926 0003179 301.0438 59.0253 15.36599655 01
| Epoch (UTC): | 25 May 2026 01:03:04 |
| Eccentricity: | 0.0003179 |
| inclination: | 53.1568° |
| perigee height: | 454 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 259.0926° |
| argument of perigee: | 301.0438° |
| revolutions per day: | 15.36599655 |
| mean anomaly at epoch: | 59.0253° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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