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 18214U 87062A 23150.04590032 .00004566 00000-0 25524-3 0 9995
2 18214 82.5180 132.5155 0029596 18.4960 341.7339 15.12871479956110
| Epoch (UTC): | 30 May 2023 01:06:05 |
| Eccentricity: | 0.0029596 |
| inclination: | 82.5180° |
| perigee height: | 507 km |
| apogee height: | 548 km |
| right ascension of ascending node: | 132.5155° |
| argument of perigee: | 18.4960° |
| revolutions per day: | 15.12871479 |
| mean anomaly at epoch: | 341.7339° |
| orbit number at epoch: | 95611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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