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 63649U 26145.40716830 +.00000000 +00000-0 +93027-3 0 00002
2 63649 42.9980 291.6200 0000085 70.6828 289.4032 15.27600112 09
| Epoch (UTC): | 25 May 2026 09:46:19 |
| Eccentricity: | 0.0000085 |
| inclination: | 42.9980° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 291.6200° |
| argument of perigee: | 70.6828° |
| revolutions per day: | 15.27600112 |
| mean anomaly at epoch: | 289.4032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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