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 63233U 26145.27520183 +.00000000 +00000-0 +19946-3 0 00008
2 63233 97.3945 37.5199 0004382 231.1376 128.9470 15.21504387 07
| Epoch (UTC): | 25 May 2026 06:36:17 |
| Eccentricity: | 0.0004382 |
| inclination: | 97.3945° |
| perigee height: | 498 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 37.5199° |
| argument of perigee: | 231.1376° |
| revolutions per day: | 15.21504387 |
| mean anomaly at epoch: | 128.9470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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