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 35756U 26106.75659007 +.00000000 +00000-0 +00000-0 0 00003
2 35756 0.8577 270.2650 0003060 111.4702 251.6619 1.00270511 09
| Epoch (UTC): | 16 April 2026 18:09:29 |
| Eccentricity: | 0.0003060 |
| inclination: | 0.8577° |
| perigee height: | 35774 km |
| apogee height: | 35800 km |
| right ascension of ascending node: | 270.2650° |
| argument of perigee: | 111.4702° |
| revolutions per day: | 1.00270511 |
| mean anomaly at epoch: | 251.6619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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