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 47366U 26145.07039530 +.00000000 +00000-0 +16134-3 0 00002
2 47366 53.1603 67.3470 0001219 91.8067 268.3074 15.31715952 06
| Epoch (UTC): | 25 May 2026 01:41:22 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 67.3470° |
| argument of perigee: | 91.8067° |
| revolutions per day: | 15.31715952 |
| mean anomaly at epoch: | 268.3074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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