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 18215U 87062B 23033.43522118 .00000649 00000-0 75656-4 0 9999
2 18215 82.5145 156.0816 0020202 185.2987 241.9571 14.83594479899680
| Epoch (UTC): | 02 February 2023 10:26:43 |
| Eccentricity: | 0.0020202 |
| inclination: | 82.5145° |
| perigee height: | 604 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 156.0816° |
| argument of perigee: | 185.2987° |
| revolutions per day: | 14.83594479 |
| mean anomaly at epoch: | 241.9571° |
| orbit number at epoch: | 89968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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