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 64763U 26145.26786998 +.00000000 +00000-0 +51050-3 0 00006
2 64763 53.1596 246.5293 0001089 82.5892 277.5235 15.34413813 04
| Epoch (UTC): | 25 May 2026 06:25:43 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 246.5293° |
| argument of perigee: | 82.5892° |
| revolutions per day: | 15.34413813 |
| mean anomaly at epoch: | 277.5235° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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