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 15331U 84105A 22145.54012852 .00004609 00000-0 23948-3 0 9990
2 15331 82.5378 355.9189 0014223 166.1061 194.0566 15.15764711 54403
| Epoch (UTC): | 25 May 2022 12:57:47 |
| Eccentricity: | 0.0014223 |
| inclination: | 82.5378° |
| perigee height: | 509 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 355.9189° |
| argument of perigee: | 166.1061° |
| revolutions per day: | 15.15764711 |
| mean anomaly at epoch: | 194.0566° |
| orbit number at epoch: | 5440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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