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 47386U 26145.40223578 +.00000000 +00000-0 +14503-3 0 00006
2 47386 53.1591 40.3709 0001164 91.4955 268.6179 15.30195748 04
| Epoch (UTC): | 25 May 2026 09:39:13 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.3709° |
| argument of perigee: | 91.4955° |
| revolutions per day: | 15.30195748 |
| mean anomaly at epoch: | 268.6179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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