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 00733U 26066.77782499 +.00000000 +00000-0 +12819-3 0 00003
2 00733 99.1227 80.0111 0031921 263.8390 95.9156 14.34018867 00
| Epoch (UTC): | 07 March 2026 18:40:04 |
| Eccentricity: | 0.0031921 |
| inclination: | 99.1227° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 80.0111° |
| argument of perigee: | 263.8390° |
| revolutions per day: | 14.34018867 |
| mean anomaly at epoch: | 95.9156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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