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 42662U 26145.60563279 +.00000000 +00000-0 +00000-0 0 00009
2 42662 0.1005 91.4288 0003723 144.2943 335.9937 1.00274772 01
| Epoch (UTC): | 25 May 2026 14:32:06 |
| Eccentricity: | 0.0003723 |
| inclination: | 0.1005° |
| perigee height: | 35770 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 91.4288° |
| argument of perigee: | 144.2943° |
| revolutions per day: | 1.00274772 |
| mean anomaly at epoch: | 335.9937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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