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 data is extracted from the following two-line orbital elements,
1 33499U 09002H 23092.24757136 .00002522 00000-0 36674-3 0 9990
2 33499 98.1828 343.5693 0010141 107.7451 252.4866 14.76817574763280
| Epoch (UTC): | 02 April 2023 05:56:30 |
| Eccentricity: | 0.0010141 |
| inclination: | 98.1828° |
| perigee height: | 632 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 343.5693° |
| argument of perigee: | 107.7451° |
| revolutions per day: | 14.76817574 |
| mean anomaly at epoch: | 252.4866° |
| orbit number at epoch: | 76328 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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