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 00020U 26047.24242536 +.00000000 +00000-0 +39536-3 0 00001
2 00020 33.3445 342.3790 1638176 125.1878 251.3313 11.61826848 01
| Epoch (UTC): | 16 February 2026 05:49:05 |
| Eccentricity: | 0.1638176 |
| inclination: | 33.3445° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 342.3790° |
| argument of perigee: | 125.1878° |
| revolutions per day: | 11.61826848 |
| mean anomaly at epoch: | 251.3313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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