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 63006U 26145.33335647 +.00000000 +00000-0 +38114-3 0 00000
2 63006 43.0004 93.7452 0001517 271.5602 86.0778 15.70811682 00
| Epoch (UTC): | 25 May 2026 08:00:01 |
| Eccentricity: | 0.0001517 |
| inclination: | 43.0004° |
| perigee height: | 356 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 93.7452° |
| argument of perigee: | 271.5602° |
| revolutions per day: | 15.70811682 |
| mean anomaly at epoch: | 86.0778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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