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 47380U 26145.63554807 +.00000000 +00000-0 +69453-3 0 00001
2 47380 53.0562 22.8113 0003339 206.6381 153.4466 15.74056227 04
| Epoch (UTC): | 25 May 2026 15:15:11 |
| Eccentricity: | 0.0003339 |
| inclination: | 53.0562° |
| perigee height: | 345 km |
| apogee height: | 350 km |
| right ascension of ascending node: | 22.8113° |
| argument of perigee: | 206.6381° |
| revolutions per day: | 15.74056227 |
| mean anomaly at epoch: | 153.4466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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