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 47346U 26145.51743721 +.00000000 +00000-0 -45900-4 0 00008
2 47346 90.1296 241.5478 0004482 102.6651 257.4982 13.16658325 00
| Epoch (UTC): | 25 May 2026 12:25:06 |
| Eccentricity: | 0.0004482 |
| inclination: | 90.1296° |
| perigee height: | 1194 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 241.5478° |
| argument of perigee: | 102.6651° |
| revolutions per day: | 13.16658325 |
| mean anomaly at epoch: | 257.4982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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