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 63231U 26145.11897978 +.00000000 +00000-0 +29477-3 0 00008
2 63231 97.3949 38.9102 0003534 211.6719 148.4307 15.25731485 01
| Epoch (UTC): | 25 May 2026 02:51:19 |
| Eccentricity: | 0.0003534 |
| inclination: | 97.3949° |
| perigee height: | 486 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 38.9102° |
| argument of perigee: | 211.6719° |
| revolutions per day: | 15.25731485 |
| mean anomaly at epoch: | 148.4307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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