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 26106.79747262 +.00000000 +00000-0 +68313-4 0 00004
2 06236 101.9971 129.5697 0003939 266.3441 269.2387 12.53210321 03
| Epoch (UTC): | 16 April 2026 19:08:21 |
| Eccentricity: | 0.0003939 |
| inclination: | 101.9971° |
| perigee height: | 1448 km |
| apogee height: | 1454 km |
| right ascension of ascending node: | 129.5697° |
| argument of perigee: | 266.3441° |
| revolutions per day: | 12.53210321 |
| mean anomaly at epoch: | 269.2387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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