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 42470U 26100.25451588 +.00000000 +00000-0 +11032-2 0 00006
2 42470 21.2568 301.3491 6691611 336.7947 3.4697 2.93447728 08
| Epoch (UTC): | 10 April 2026 06:06:30 |
| Eccentricity: | 0.6691611 |
| inclination: | 21.2568° |
| perigee height: | 440 km |
| apogee height: | 28021 km |
| right ascension of ascending node: | 301.3491° |
| argument of perigee: | 336.7947° |
| revolutions per day: | 2.93447728 |
| mean anomaly at epoch: | 3.4697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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