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 26070.75490926 +.00000000 +00000-0 +11716-3 0 00002
2 00733 99.1225 84.2049 0031989 251.9325 107.8372 14.34021575 07
| Epoch (UTC): | 11 March 2026 18:07:04 |
| Eccentricity: | 0.0031989 |
| inclination: | 99.1225° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 84.2049° |
| argument of perigee: | 251.9325° |
| revolutions per day: | 14.34021575 |
| mean anomaly at epoch: | 107.8372° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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