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 20509U 90017B 22145.83263985 .00000053 00000-0 39010-4 0 9996
2 20509 82.9549 69.6504 0043354 163.2259 197.0343 13.75629496618286
| Epoch (UTC): | 25 May 2022 19:59:00 |
| Eccentricity: | 0.0043354 |
| inclination: | 82.9549° |
| perigee height: | 947 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 69.6504° |
| argument of perigee: | 163.2259° |
| revolutions per day: | 13.75629496 |
| mean anomaly at epoch: | 197.0343° |
| orbit number at epoch: | 61828 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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