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 63946U 26145.55461995 +.00000000 +00000-0 +28123-3 0 00002
2 63946 70.0022 80.7526 0002547 271.3820 88.7048 14.98340118 04
| Epoch (UTC): | 25 May 2026 13:18:39 |
| Eccentricity: | 0.0002547 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.7526° |
| argument of perigee: | 271.3820° |
| revolutions per day: | 14.98340118 |
| mean anomaly at epoch: | 88.7048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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