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 42959U 26145.66123560 +.00000000 +00000-0 -49556-5 0 00004
2 42959 86.3984 34.6652 0002237 84.7109 275.4342 14.34217461 08
| Epoch (UTC): | 25 May 2026 15:52:10 |
| Eccentricity: | 0.0002237 |
| inclination: | 86.3984° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 34.6652° |
| argument of perigee: | 84.7109° |
| revolutions per day: | 14.34217461 |
| mean anomaly at epoch: | 275.4342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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