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 26073.61561624 +.00000000 +00000-0 +11701-3 0 00008
2 00733 99.1223 87.2216 0032045 243.3575 116.4324 14.34023578 08
| Epoch (UTC): | 14 March 2026 14:46:29 |
| Eccentricity: | 0.0032045 |
| inclination: | 99.1223° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 87.2216° |
| argument of perigee: | 243.3575° |
| revolutions per day: | 14.34023578 |
| mean anomaly at epoch: | 116.4324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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