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 51889U 26145.05636551 +.00000000 +00000-0 -71734-4 0 00000
2 51889 53.2147 16.2974 0001599 102.0323 258.0848 15.08844356 08
| Epoch (UTC): | 25 May 2026 01:21:09 |
| Eccentricity: | 0.0001599 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 16.2974° |
| argument of perigee: | 102.0323° |
| revolutions per day: | 15.08844356 |
| mean anomaly at epoch: | 258.0848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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