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 26070U 26020.19220457 +.00000000 +00000-0 -25782-4 0 00007
2 26070 71.0003 199.8074 0018822 256.9747 102.9275 14.15812302 00
| Epoch (UTC): | 20 January 2026 04:36:46 |
| Eccentricity: | 0.0018822 |
| inclination: | 71.0003° |
| perigee height: | 826 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 199.8074° |
| argument of perigee: | 256.9747° |
| revolutions per day: | 14.15812302 |
| mean anomaly at epoch: | 102.9275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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