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 26064.56143884 +.00000000 +00000-0 +89070-4 0 00003
2 26070 71.0012 106.5183 0017079 195.9469 164.1119 14.15825328 01
| Epoch (UTC): | 05 March 2026 13:28:28 |
| Eccentricity: | 0.0017079 |
| inclination: | 71.0012° |
| perigee height: | 827 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 106.5183° |
| argument of perigee: | 195.9469° |
| revolutions per day: | 14.15825328 |
| mean anomaly at epoch: | 164.1119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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