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 17589U 26039.41183696 +.00000000 +00000-0 +54930-4 0 00006
2 17589 70.9213 27.5496 0024889 253.7329 106.1054 14.13056433 06
| Epoch (UTC): | 08 February 2026 09:53:02 |
| Eccentricity: | 0.0024889 |
| inclination: | 70.9213° |
| perigee height: | 831 km |
| apogee height: | 867 km |
| right ascension of ascending node: | 27.5496° |
| argument of perigee: | 253.7329° |
| revolutions per day: | 14.13056433 |
| mean anomaly at epoch: | 106.1054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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