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 61889U 26145.33214398 +.00000000 +00000-0 +36172-4 0 00009
2 61889 53.1602 130.2487 0001170 88.8570 271.2566 15.34387340 08
| Epoch (UTC): | 25 May 2026 07:58:17 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 130.2487° |
| argument of perigee: | 88.8570° |
| revolutions per day: | 15.34387340 |
| mean anomaly at epoch: | 271.2566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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