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 63638U 26145.41873573 +.00000000 +00000-0 +72783-3 0 00005
2 63638 42.9966 291.7069 0000349 303.6094 56.4724 15.27593964 08
| Epoch (UTC): | 25 May 2026 10:02:58 |
| Eccentricity: | 0.0000349 |
| inclination: | 42.9966° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 291.7069° |
| argument of perigee: | 303.6094° |
| revolutions per day: | 15.27593964 |
| mean anomaly at epoch: | 56.4724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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