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 26111.96841963 +.00000000 +00000-0 +79683-4 0 00002
2 26070 71.0044 6.8361 0014682 119.6888 240.5699 14.15828703 03
| Epoch (UTC): | 21 April 2026 23:14:31 |
| Eccentricity: | 0.0014682 |
| inclination: | 71.0044° |
| perigee height: | 829 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 6.8361° |
| argument of perigee: | 119.6888° |
| revolutions per day: | 14.15828703 |
| mean anomaly at epoch: | 240.5699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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