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 33490U 09001A 22262.97786972 0.00000000 00000-0 00000-0 0 01
2 33490 6.8191 35.0525 0010442 315.1798 44.7069 1.00270000 01
| Epoch (UTC): | 19 September 2022 23:28:07 |
| Eccentricity: | 0.0010442 |
| inclination: | 6.8191° |
| perigee height: | 35742 km |
| apogee height: | 35831 km |
| right ascension of ascending node: | 35.0525° |
| argument of perigee: | 315.1798° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 44.7069° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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