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 26038.99461699 +.00000000 +00000-0 +79770-4 0 00005
2 04589 74.0575 233.3966 0020061 8.7004 351.4496 14.43280475 06
| Epoch (UTC): | 07 February 2026 23:52:14 |
| Eccentricity: | 0.0020061 |
| inclination: | 74.0575° |
| perigee height: | 733 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 233.3966° |
| argument of perigee: | 8.7004° |
| revolutions per day: | 14.43280475 |
| mean anomaly at epoch: | 351.4496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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