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 63217U 26145.14398839 +.00000000 +00000-0 +53892-3 0 00005
2 63217 97.3906 41.0991 0002689 157.2132 202.9230 15.32981102 05
| Epoch (UTC): | 25 May 2026 03:27:20 |
| Eccentricity: | 0.0002689 |
| inclination: | 97.3906° |
| perigee height: | 465 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 41.0991° |
| argument of perigee: | 157.2132° |
| revolutions per day: | 15.32981102 |
| mean anomaly at epoch: | 202.9230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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