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 64053U 26145.63059633 +.00000000 +00000-0 +16938-3 0 00004
2 64053 97.3811 217.6347 0001828 219.1266 140.9837 15.18828593 07
| Epoch (UTC): | 25 May 2026 15:08:03 |
| Eccentricity: | 0.0001828 |
| inclination: | 97.3811° |
| perigee height: | 508 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 217.6347° |
| argument of perigee: | 219.1266° |
| revolutions per day: | 15.18828593 |
| mean anomaly at epoch: | 140.9837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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