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 04589U 70086B 22143.75200363 .00000251 00000-0 84762-4 0 9994
2 04589 74.0605 225.5822 0021212 343.5068 16.5395 14.41743959706338
| Epoch (UTC): | 23 May 2022 18:02:53 |
| Eccentricity: | 0.0021212 |
| inclination: | 74.0605° |
| perigee height: | 737 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 225.5822° |
| argument of perigee: | 343.5068° |
| revolutions per day: | 14.41743959 |
| mean anomaly at epoch: | 16.5395° |
| orbit number at epoch: | 70633 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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