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 51467U 26145.44276764 +.00000000 +00000-0 +32465-4 0 00008
2 51467 53.2131 294.5603 0001225 85.6387 274.4745 15.08840551 06
| Epoch (UTC): | 25 May 2026 10:37:35 |
| Eccentricity: | 0.0001225 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.5603° |
| argument of perigee: | 85.6387° |
| revolutions per day: | 15.08840551 |
| mean anomaly at epoch: | 274.4745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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