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 06235U 26121.97035012 +.00000000 +00000-0 +46581-4 0 00006
2 06235 102.0105 140.0311 0003689 256.3192 112.4167 12.53213544 03
| Epoch (UTC): | 01 May 2026 23:17:18 |
| Eccentricity: | 0.0003689 |
| inclination: | 102.0105° |
| perigee height: | 1448 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 140.0311° |
| argument of perigee: | 256.3192° |
| revolutions per day: | 12.53213544 |
| mean anomaly at epoch: | 112.4167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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