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 26075.98790869 +.00000000 +00000-0 +87406-4 0 00001
2 00733 99.1220 89.7231 0032094 236.2698 123.5425 14.34024531 01
| Epoch (UTC): | 16 March 2026 23:42:35 |
| Eccentricity: | 0.0032094 |
| inclination: | 99.1220° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 89.7231° |
| argument of perigee: | 236.2698° |
| revolutions per day: | 14.34024531 |
| mean anomaly at epoch: | 123.5425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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