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 06236U 26053.79246750 +.00000000 +00000-0 -18323-4 0 00008
2 06236 102.0040 76.0215 0004273 12.8612 168.7364 12.53209160 07
| Epoch (UTC): | 22 February 2026 19:01:09 |
| Eccentricity: | 0.0004273 |
| inclination: | 102.0040° |
| perigee height: | 1448 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 76.0215° |
| argument of perigee: | 12.8612° |
| revolutions per day: | 12.53209160 |
| mean anomaly at epoch: | 168.7364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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