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 47623U 26145.66668980 +.00000000 +00000-0 +62378-3 0 00001
2 47623 53.0326 303.5738 0006231 236.4301 268.1050 15.83411982 07
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0006231 |
| inclination: | 53.0326° |
| perigee height: | 317 km |
| apogee height: | 325 km |
| right ascension of ascending node: | 303.5738° |
| argument of perigee: | 236.4301° |
| revolutions per day: | 15.83411982 |
| mean anomaly at epoch: | 268.1050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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