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 26073.46350521 +.00000000 +00000-0 -75490-4 0 00002
2 26070 71.0004 87.7988 0016486 183.0564 177.0461 14.15824818 06
| Epoch (UTC): | 14 March 2026 11:07:26 |
| Eccentricity: | 0.0016486 |
| inclination: | 71.0004° |
| perigee height: | 828 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 87.7988° |
| argument of perigee: | 183.0564° |
| revolutions per day: | 14.15824818 |
| mean anomaly at epoch: | 177.0461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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