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 64101U 26145.10355519 +.00000000 +00000-0 +57982-3 0 00006
2 64101 53.1588 31.7006 0001148 73.9254 286.1873 15.31710355 01
| Epoch (UTC): | 25 May 2026 02:29:07 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 31.7006° |
| argument of perigee: | 73.9254° |
| revolutions per day: | 15.31710355 |
| mean anomaly at epoch: | 286.1873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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