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 26066.18641894 +.00000000 +00000-0 +33050-4 0 00004
2 26070 71.0011 103.1015 0016954 193.7432 166.3232 14.15825660 03
| Epoch (UTC): | 07 March 2026 04:28:26 |
| Eccentricity: | 0.0016954 |
| inclination: | 71.0011° |
| perigee height: | 827 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 103.1015° |
| argument of perigee: | 193.7432° |
| revolutions per day: | 14.15825660 |
| mean anomaly at epoch: | 166.3232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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