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 33498U 09002G 22176.83649540 .00000958 00000-0 13380-3 0 9995
2 33498 98.1686 68.9806 0009613 219.5565 140.4945 14.80012557723097
| Epoch (UTC): | 25 June 2022 20:04:33 |
| Eccentricity: | 0.0009613 |
| inclination: | 98.1686° |
| perigee height: | 622 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 68.9806° |
| argument of perigee: | 219.5565° |
| revolutions per day: | 14.80012557 |
| mean anomaly at epoch: | 140.4945° |
| orbit number at epoch: | 72309 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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