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 42070U 26038.88776865 +.00000000 +00000-0 +00000-0 0 00000
2 42070 0.0194 101.5065 0001912 215.5273 30.6389 1.00272374 00
| Epoch (UTC): | 07 February 2026 21:18:23 |
| Eccentricity: | 0.0001912 |
| inclination: | 0.0194° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 101.5065° |
| argument of perigee: | 215.5273° |
| revolutions per day: | 1.00272374 |
| mean anomaly at epoch: | 30.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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