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 26064.26597949 +.00000000 +00000-0 +13098-3 0 00009
2 00733 99.1227 77.3623 0031906 271.3525 88.4003 14.34017210 03
| Epoch (UTC): | 05 March 2026 06:23:00 |
| Eccentricity: | 0.0031906 |
| inclination: | 99.1227° |
| perigee height: | 756 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 77.3623° |
| argument of perigee: | 271.3525° |
| revolutions per day: | 14.34017210 |
| mean anomaly at epoch: | 88.4003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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