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 63235U 26145.24348044 +.00000000 +00000-0 +28277-3 0 00008
2 63235 97.3896 38.0175 0004634 232.4821 127.5996 15.23619117 01
| Epoch (UTC): | 25 May 2026 05:50:36 |
| Eccentricity: | 0.0004634 |
| inclination: | 97.3896° |
| perigee height: | 492 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 38.0175° |
| argument of perigee: | 232.4821° |
| revolutions per day: | 15.23619117 |
| mean anomaly at epoch: | 127.5996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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