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 33505U 09003B 22228.30815344 .00001629 00000-0 96140-4 0 9994
2 33505 82.3907 167.0705 0024784 177.1457 182.9919 15.10620096745410
| Epoch (UTC): | 16 August 2022 07:23:44 |
| Eccentricity: | 0.0024784 |
| inclination: | 82.3907° |
| perigee height: | 517 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 167.0705° |
| argument of perigee: | 177.1457° |
| revolutions per day: | 15.10620096 |
| mean anomaly at epoch: | 182.9919° |
| orbit number at epoch: | 74541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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