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 32287U 07054A 22059.59897852 0.00000000 00000-0 00000-0 0 02
2 32287 7.4919 61.5637 0007819 230.0498 130.1018 1.00372228 02
| Epoch (UTC): | 28 February 2022 14:22:31 |
| Eccentricity: | 0.0007819 |
| inclination: | 7.4919° |
| perigee height: | 35725 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 61.5637° |
| argument of perigee: | 230.0498° |
| revolutions per day: | 1.00372228 |
| mean anomaly at epoch: | 130.1018° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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