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 64051U 26088.16888483 +.00000000 +00000-0 +28796-3 0 00004
2 64051 97.3876 161.3096 0004004 111.5236 248.6425 15.17771891 09
| Epoch (UTC): | 29 March 2026 04:03:11 |
| Eccentricity: | 0.0004004 |
| inclination: | 97.3876° |
| perigee height: | 510 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 161.3096° |
| argument of perigee: | 111.5236° |
| revolutions per day: | 15.17771891 |
| mean anomaly at epoch: | 248.6425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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