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 32953U 08025A 24261.14124437 .00000043 00000-0 23716-3 0 9997
2 32953 82.5057 32.2769 0018659 263.2722 96.6235 12.43148257740541
| Epoch (UTC): | 17 September 2024 03:23:23 |
| Eccentricity: | 0.0018659 |
| inclination: | 82.5057° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 32.2769° |
| argument of perigee: | 263.2722° |
| revolutions per day: | 12.43148257 |
| mean anomaly at epoch: | 96.6235° |
| orbit number at epoch: | 74054 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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