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 4384U 70036B 23265.52911990 .00000000 00000-0 11982-3 0 9993
2 4384 74.0255 277.0837 0054102 333.3334 144.8121 12.39230953416371
| Epoch (UTC): | 22 September 2023 12:41:55 |
| Eccentricity: | 0.0054102 |
| inclination: | 74.0255° |
| perigee height: | 1467 km |
| apogee height: | 1552 km |
| right ascension of ascending node: | 277.0837° |
| argument of perigee: | 333.3334° |
| revolutions per day: | 12.39230953 |
| mean anomaly at epoch: | 144.8121° |
| orbit number at epoch: | 41637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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