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 63664U 26145.48448762 +.00000000 +00000-0 +11350-2 0 00001
2 63664 43.0004 175.1685 0001381 247.6701 112.4020 15.70864686 02
| Epoch (UTC): | 25 May 2026 11:37:39 |
| Eccentricity: | 0.0001381 |
| inclination: | 43.0004° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 175.1685° |
| argument of perigee: | 247.6701° |
| revolutions per day: | 15.70864686 |
| mean anomaly at epoch: | 112.4020° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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