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 03047U 67116A 22229.29832207 .00000184 00000-0 48645-4 0 9999
2 03047 74.0131 156.5580 0009375 302.1042 57.9211 14.55810976894785
| Epoch (UTC): | 17 August 2022 07:09:35 |
| Eccentricity: | 0.0009375 |
| inclination: | 74.0131° |
| perigee height: | 700 km |
| apogee height: | 713 km |
| right ascension of ascending node: | 156.5580° |
| argument of perigee: | 302.1042° |
| revolutions per day: | 14.55810976 |
| mean anomaly at epoch: | 57.9211° |
| orbit number at epoch: | 89478 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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