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 63229U 26145.25728897 +.00000000 +00000-0 +19544-3 0 00007
2 63229 97.3980 38.1717 0003509 212.5420 147.5601 15.22248988 03
| Epoch (UTC): | 25 May 2026 06:10:29 |
| Eccentricity: | 0.0003509 |
| inclination: | 97.3980° |
| perigee height: | 497 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 38.1717° |
| argument of perigee: | 212.5420° |
| revolutions per day: | 15.22248988 |
| mean anomaly at epoch: | 147.5601° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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