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 63234U 26145.26549979 +.00000000 +00000-0 +18178-3 0 00008
2 63234 97.4017 38.3124 0005341 220.5281 139.5558 15.22196275 08
| Epoch (UTC): | 25 May 2026 06:22:19 |
| Eccentricity: | 0.0005341 |
| inclination: | 97.4017° |
| perigee height: | 496 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 38.3124° |
| argument of perigee: | 220.5281° |
| revolutions per day: | 15.22196275 |
| mean anomaly at epoch: | 139.5558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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