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 47604U 26145.66668980 +.00000000 +00000-0 +74643-3 0 00008
2 47604 53.0378 313.0276 0003392 301.9283 115.4948 15.84575269 08
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0003392 |
| inclination: | 53.0378° |
| perigee height: | 315 km |
| apogee height: | 320 km |
| right ascension of ascending node: | 313.0276° |
| argument of perigee: | 301.9283° |
| revolutions per day: | 15.84575269 |
| mean anomaly at epoch: | 115.4948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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