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 00053U 60009E 22027.30467333 .00000005 00000-0 89410-3 0 9995
2 00053 47.2738 243.0432 0100098 22.0488 338.4565 12.17269531740294
| Epoch (UTC): | 27 January 2022 07:18:43 |
| Eccentricity: | 0.0100098 |
| inclination: | 47.2738° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 243.0432° |
| argument of perigee: | 22.0488° |
| revolutions per day: | 12.17269531 |
| mean anomaly at epoch: | 338.4565° |
| orbit number at epoch: | 74029 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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