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 51984U 26145.15669353 +.00000000 +00000-0 +31775-4 0 00003
2 51984 53.2153 55.9314 0001443 91.7403 268.3755 15.08841324 03
| Epoch (UTC): | 25 May 2026 03:45:38 |
| Eccentricity: | 0.0001443 |
| inclination: | 53.2153° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.9314° |
| argument of perigee: | 91.7403° |
| revolutions per day: | 15.08841324 |
| mean anomaly at epoch: | 268.3755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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