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 26039.82639205 +.00000000 +00000-0 +77298-4 0 00001
2 04589 74.0575 231.8536 0020095 6.9305 353.2126 14.43280875 07
| Epoch (UTC): | 08 February 2026 19:50:00 |
| Eccentricity: | 0.0020095 |
| inclination: | 74.0575° |
| perigee height: | 733 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 231.8536° |
| argument of perigee: | 6.9305° |
| revolutions per day: | 14.43280875 |
| mean anomaly at epoch: | 353.2126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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