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 26104.04952865 +.00000000 +00000-0 +12731-3 0 00009
2 06236 101.9975 126.7942 0003936 271.9712 111.3433 12.53210256 05
| Epoch (UTC): | 14 April 2026 01:11:19 |
| Eccentricity: | 0.0003936 |
| inclination: | 101.9975° |
| perigee height: | 1448 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 126.7942° |
| argument of perigee: | 271.9712° |
| revolutions per day: | 12.53210256 |
| mean anomaly at epoch: | 111.3433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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