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 26064.89394102 +.00000000 +00000-0 +11218-3 0 00006
2 00733 99.1227 78.0245 0031916 269.4934 90.2592 14.34017361 05
| Epoch (UTC): | 05 March 2026 21:27:16 |
| Eccentricity: | 0.0031916 |
| inclination: | 99.1227° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 78.0245° |
| argument of perigee: | 269.4934° |
| revolutions per day: | 14.34017361 |
| mean anomaly at epoch: | 90.2592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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