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 53U 60009E 23033.12892185 -.00000019 00000-0 65735-3 0 9990
2 53 47.2744 179.4198 0098886 38.1792 322.5950 12.17289341785460
| Epoch (UTC): | 02 February 2023 03:05:38 |
| Eccentricity: | 0.0098886 |
| inclination: | 47.2744° |
| perigee height: | 1525 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 179.4198° |
| argument of perigee: | 38.1792° |
| revolutions per day: | 12.17289341 |
| mean anomaly at epoch: | 322.5950° |
| orbit number at epoch: | 78546 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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