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 47695U 26145.57106235 +.00000000 +00000-0 +51854-4 0 00008
2 47695 63.4028 255.8227 0175194 0.8730 359.2569 13.45447561 01
| Epoch (UTC): | 25 May 2026 13:42:19 |
| Eccentricity: | 0.0175194 |
| inclination: | 63.4028° |
| perigee height: | 958 km |
| apogee height: | 1220 km |
| right ascension of ascending node: | 255.8227° |
| argument of perigee: | 0.8730° |
| revolutions per day: | 13.45447561 |
| mean anomaly at epoch: | 359.2569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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