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 63678U 26145.49387882 +.00000000 +00000-0 +66829-3 0 00004
2 63678 43.0004 317.3873 0000708 211.3192 148.7618 15.27605714 02
| Epoch (UTC): | 25 May 2026 11:51:11 |
| Eccentricity: | 0.0000708 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 317.3873° |
| argument of perigee: | 211.3192° |
| revolutions per day: | 15.27605714 |
| mean anomaly at epoch: | 148.7618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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