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 47388U 26145.51399705 +.00000000 +00000-0 +35124-4 0 00009
2 47388 53.1619 68.9681 0001645 77.7059 282.4126 15.31702523 00
| Epoch (UTC): | 25 May 2026 12:20:09 |
| Eccentricity: | 0.0001645 |
| inclination: | 53.1619° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 68.9681° |
| argument of perigee: | 77.7059° |
| revolutions per day: | 15.31702523 |
| mean anomaly at epoch: | 282.4126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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