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 22183.10699505 .00000024 00000-0 10000-3 0 9998
2 32953 82.5020 174.8227 0018223 225.9558 134.0021 12.43111463640157
| Epoch (UTC): | 02 July 2022 02:34:04 |
| Eccentricity: | 0.0018223 |
| inclination: | 82.5020° |
| perigee height: | 1479 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 174.8227° |
| argument of perigee: | 225.9558° |
| revolutions per day: | 12.43111463 |
| mean anomaly at epoch: | 134.0021° |
| orbit number at epoch: | 64015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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