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 26068.29593103 +.00000000 +00000-0 +20343-4 0 00000
2 06236 102.0024 90.6753 0004121 344.6456 82.4669 12.53209475 01
| Epoch (UTC): | 09 March 2026 07:06:08 |
| Eccentricity: | 0.0004121 |
| inclination: | 102.0024° |
| perigee height: | 1448 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 90.6753° |
| argument of perigee: | 344.6456° |
| revolutions per day: | 12.53209475 |
| mean anomaly at epoch: | 82.4669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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