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 26071.48526719 +.00000000 +00000-0 -61237-4 0 00000
2 26070 71.0006 91.9589 0016616 186.1025 173.9898 14.15825371 07
| Epoch (UTC): | 12 March 2026 11:38:47 |
| Eccentricity: | 0.0016616 |
| inclination: | 71.0006° |
| perigee height: | 828 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 91.9589° |
| argument of perigee: | 186.1025° |
| revolutions per day: | 14.15825371 |
| mean anomaly at epoch: | 173.9898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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