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 63489U 26145.27759964 +.00000000 +00000-0 +28496-3 0 00002
2 63489 97.4029 38.0957 0004456 244.0723 116.0055 15.22792032 07
| Epoch (UTC): | 25 May 2026 06:39:44 |
| Eccentricity: | 0.0004456 |
| inclination: | 97.4029° |
| perigee height: | 494 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 38.0957° |
| argument of perigee: | 244.0723° |
| revolutions per day: | 15.22792032 |
| mean anomaly at epoch: | 116.0055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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