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 15332U 84105B 23152.52361602 .00000541 00000-0 61909-4 0 9999
2 15332 82.5328 314.1810 0021764 38.6282 23.3080 14.83994595 68019
| Epoch (UTC): | 01 June 2023 12:34:00 |
| Eccentricity: | 0.0021764 |
| inclination: | 82.5328° |
| perigee height: | 601 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 314.1810° |
| argument of perigee: | 38.6282° |
| revolutions per day: | 14.83994595 |
| mean anomaly at epoch: | 23.3080° |
| orbit number at epoch: | 6801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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