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 51893U 26145.37648913 +.00000000 +00000-0 +18086-3 0 00004
2 51893 53.2182 14.8607 0001296 87.5413 272.5727 15.08866729 05
| Epoch (UTC): | 25 May 2026 09:02:08 |
| Eccentricity: | 0.0001296 |
| inclination: | 53.2182° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 14.8607° |
| argument of perigee: | 87.5413° |
| revolutions per day: | 15.08866729 |
| mean anomaly at epoch: | 272.5727° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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