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 26040.93542497 +.00000000 +00000-0 +77629-4 0 00009
2 04589 74.0575 229.7963 0020138 4.6043 355.5295 14.43281513 01
| Epoch (UTC): | 09 February 2026 22:27:00 |
| Eccentricity: | 0.0020138 |
| inclination: | 74.0575° |
| perigee height: | 733 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 229.7963° |
| argument of perigee: | 4.6043° |
| revolutions per day: | 14.43281513 |
| mean anomaly at epoch: | 355.5295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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