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 47753U 26145.34283475 +.00000000 +00000-0 -14200-3 0 00004
2 47753 53.1571 207.3916 0001259 97.7605 262.3539 15.31676224 06
| Epoch (UTC): | 25 May 2026 08:13:40 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1571° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 207.3916° |
| argument of perigee: | 97.7605° |
| revolutions per day: | 15.31676224 |
| mean anomaly at epoch: | 262.3539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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