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 20465U 90010A 22225.55221304 .00000965 00000-0 77237-4 0 9992
2 20465 82.4863 235.5604 0016711 69.1489 291.1522 14.99008467746184
| Epoch (UTC): | 13 August 2022 13:15:11 |
| Eccentricity: | 0.0016711 |
| inclination: | 82.4863° |
| perigee height: | 558 km |
| apogee height: | 581 km |
| right ascension of ascending node: | 235.5604° |
| argument of perigee: | 69.1489° |
| revolutions per day: | 14.99008467 |
| mean anomaly at epoch: | 291.1522° |
| orbit number at epoch: | 74618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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