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 19120U 88039B 23151.76247579 .00000123 00000-0 81334-4 0 9999
2 19120 71.0160 49.8705 0019721 94.1662 266.1717 14.19316460814919
| Epoch (UTC): | 31 May 2023 18:17:57 |
| Eccentricity: | 0.0019721 |
| inclination: | 71.0160° |
| perigee height: | 813 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 49.8705° |
| argument of perigee: | 94.1662° |
| revolutions per day: | 14.19316460 |
| mean anomaly at epoch: | 266.1717° |
| orbit number at epoch: | 81491 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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