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 23080.15740395 .00000024 00000-0 10000-3 0 9994
2 32953 82.5085 11.8433 0020311 19.0046 341.1792 12.43120759672713
| Epoch (UTC): | 21 March 2023 03:46:39 |
| Eccentricity: | 0.0020311 |
| inclination: | 82.5085° |
| perigee height: | 1477 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 11.8433° |
| argument of perigee: | 19.0046° |
| revolutions per day: | 12.43120759 |
| mean anomaly at epoch: | 341.1792° |
| orbit number at epoch: | 67271 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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