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 59881U 26145.10340927 +.00000000 +00000-0 +14396-3 0 00004
2 59881 97.4113 1.6800 0010467 290.0053 70.0055 15.20891527 07
| Epoch (UTC): | 25 May 2026 02:28:54 |
| Eccentricity: | 0.0010467 |
| inclination: | 97.4113° |
| perigee height: | 496 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 1.6800° |
| argument of perigee: | 290.0053° |
| revolutions per day: | 15.20891527 |
| mean anomaly at epoch: | 70.0055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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