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 26038.02421250 +.00000000 +00000-0 +88617-4 0 00008
2 04589 74.0574 235.1968 0020024 10.7428 349.4152 14.43280056 00
| Epoch (UTC): | 07 February 2026 00:34:51 |
| Eccentricity: | 0.0020024 |
| inclination: | 74.0574° |
| perigee height: | 733 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 235.1968° |
| argument of perigee: | 10.7428° |
| revolutions per day: | 14.43280056 |
| mean anomaly at epoch: | 349.4152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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