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 26064.61484700 +.00000000 +00000-0 +13186-3 0 00006
2 00733 99.1228 77.7302 0031910 270.3392 89.4134 14.34017472 04
| Epoch (UTC): | 05 March 2026 14:45:22 |
| Eccentricity: | 0.0031910 |
| inclination: | 99.1228° |
| perigee height: | 755 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 77.7302° |
| argument of perigee: | 270.3392° |
| revolutions per day: | 14.34017472 |
| mean anomaly at epoch: | 89.4134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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