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 is defined by the following mean orbital elements,
1 04589U 26109.27860014 +.00000000 +00000-0 +56863-4 0 00007
2 04589 74.0577 103.0278 0021300 225.8811 134.0595 14.43324970 06
| Epoch (UTC): | 19 April 2026 06:41:11 |
| Eccentricity: | 0.0021300 |
| inclination: | 74.0577° |
| perigee height: | 732 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 103.0278° |
| argument of perigee: | 225.8811° |
| revolutions per day: | 14.43324970 |
| mean anomaly at epoch: | 134.0595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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