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 42475U 26063.00445356 +.00000000 +00000-0 +17738-1 0 00006
2 42475 26.5467 332.9388 7410720 81.2038 348.5247 1.91425231 04
| Epoch (UTC): | 04 March 2026 00:06:24 |
| Eccentricity: | 0.7410720 |
| inclination: | 26.5467° |
| perigee height: | 716 km |
| apogee height: | 41326 km |
| right ascension of ascending node: | 332.9388° |
| argument of perigee: | 81.2038° |
| revolutions per day: | 1.91425231 |
| mean anomaly at epoch: | 348.5247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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