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 19650U 88102B 23150.35369821 -.00000190 00000-0 -72046-4 0 9993
2 19650 70.9977 125.2983 0012220 119.8442 240.3897 14.15890736783306
| Epoch (UTC): | 30 May 2023 08:29:19 |
| Eccentricity: | 0.0012220 |
| inclination: | 70.9977° |
| perigee height: | 830 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 125.2983° |
| argument of perigee: | 119.8442° |
| revolutions per day: | 14.15890736 |
| mean anomaly at epoch: | 240.3897° |
| orbit number at epoch: | 78330 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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