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 02144U 66031B 24276.88189650 .00002341 00000-0 68041-3 0 9995
2 02144 35.0412 197.1888 0007315 96.4829 263.6695 14.44064600 72739
| Epoch (UTC): | 02 October 2024 21:09:55 |
| Eccentricity: | 0.0007315 |
| inclination: | 35.0412° |
| perigee height: | 740 km |
| apogee height: | 750 km |
| right ascension of ascending node: | 197.1888° |
| argument of perigee: | 96.4829° |
| revolutions per day: | 14.44064600 |
| mean anomaly at epoch: | 263.6695° |
| orbit number at epoch: | 7273 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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