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 26041.90582839 +.00000000 +00000-0 +76771-4 0 00008
2 04589 74.0575 227.9962 0020182 2.5313 357.5942 14.43282031 03
| Epoch (UTC): | 10 February 2026 21:44:23 |
| Eccentricity: | 0.0020182 |
| inclination: | 74.0575° |
| perigee height: | 733 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 227.9962° |
| argument of perigee: | 2.5313° |
| revolutions per day: | 14.43282031 |
| mean anomaly at epoch: | 357.5942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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