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 33495U 09002D 22267.53087662 .00000244 00000-0 46825-4 0 9990
2 33495 98.2688 140.0745 0009155 55.8508 304.3565 14.72406095733680
| Epoch (UTC): | 24 September 2022 12:44:27 |
| Eccentricity: | 0.0009155 |
| inclination: | 98.2688° |
| perigee height: | 647 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 140.0745° |
| argument of perigee: | 55.8508° |
| revolutions per day: | 14.72406095 |
| mean anomaly at epoch: | 304.3565° |
| orbit number at epoch: | 73368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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