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 59706U 26145.19804618 +.00000000 +00000-0 +00000-0 0 00005
2 59706 53.1257 171.5268 0025977 206.7802 153.1422 2.00563277 07
| Epoch (UTC): | 25 May 2026 04:45:11 |
| Eccentricity: | 0.0025977 |
| inclination: | 53.1257° |
| perigee height: | 20113 km |
| apogee height: | 20251 km |
| right ascension of ascending node: | 171.5268° |
| argument of perigee: | 206.7802° |
| revolutions per day: | 2.00563277 |
| mean anomaly at epoch: | 153.1422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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