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 64112U 26145.41113549 +.00000000 +00000-0 +52819-3 0 00001
2 64112 53.1605 30.0600 0001302 101.5601 258.5547 15.31719809 05
| Epoch (UTC): | 25 May 2026 09:52:02 |
| Eccentricity: | 0.0001302 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 30.0600° |
| argument of perigee: | 101.5601° |
| revolutions per day: | 15.31719809 |
| mean anomaly at epoch: | 258.5547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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