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 51634U 26145.42445171 +.00000000 +00000-0 -16365-2 0 00002
2 51634 87.8849 40.8123 0001959 82.6743 277.4607 13.10372405 06
| Epoch (UTC): | 25 May 2026 10:11:12 |
| Eccentricity: | 0.0001959 |
| inclination: | 87.8849° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8123° |
| argument of perigee: | 82.6743° |
| revolutions per day: | 13.10372405 |
| mean anomaly at epoch: | 277.4607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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