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 51989U 26145.15204537 +.00000000 +00000-0 -89258-5 0 00008
2 51989 53.2144 55.8670 0001494 109.5656 250.5498 15.08843690 01
| Epoch (UTC): | 25 May 2026 03:38:56 |
| Eccentricity: | 0.0001494 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.8670° |
| argument of perigee: | 109.5656° |
| revolutions per day: | 15.08843690 |
| mean anomaly at epoch: | 250.5498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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