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 59912U 26145.49872838 +.00000000 +00000-0 +15634-3 0 00008
2 59912 44.9802 2.6276 0011202 141.7798 218.3831 13.99159073 04
| Epoch (UTC): | 25 May 2026 11:58:10 |
| Eccentricity: | 0.0011202 |
| inclination: | 44.9802° |
| perigee height: | 889 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 2.6276° |
| argument of perigee: | 141.7798° |
| revolutions per day: | 13.99159073 |
| mean anomaly at epoch: | 218.3831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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