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 15495U 85009B 22230.70547179 .00000289 00000-0 31771-4 0 9997
2 15495 82.5227 218.1468 0019057 215.1410 144.8550 14.84065371 8866
| Epoch (UTC): | 18 August 2022 16:55:52 |
| Eccentricity: | 0.0019057 |
| inclination: | 82.5227° |
| perigee height: | 603 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 218.1468° |
| argument of perigee: | 215.1410° |
| revolutions per day: | 14.84065371 |
| mean anomaly at epoch: | 144.8550° |
| orbit number at epoch: | 886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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