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 is defined by the following mean orbital elements,
1 44419U 19038F 24161.30699751 .14138513 27681-5 32002-3 0 9992
2 44419 97.6384 170.8746 0011571 240.3842 119.6307 16.45656077273974
| Epoch (UTC): | 09 June 2024 07:22:04 |
| Eccentricity: | 0.0011571 |
| inclination: | 97.6384° |
| perigee height: | 143 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 170.8746° |
| argument of perigee: | 240.3842° |
| revolutions per day: | 16.45656077 |
| mean anomaly at epoch: | 119.6307° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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