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 70469U 26108.74701389 +.00000000 +00000-0 -36754-2 0 00003
2 70469 97.2876 330.5037 0001427 84.0132 112.2864 16.03869813 09
| Epoch (UTC): | 18 April 2026 17:55:42 |
| Eccentricity: | 0.0001427 |
| inclination: | 97.2876° |
| perigee height: | 263 km |
| apogee height: | 265 km |
| right ascension of ascending node: | 330.5037° |
| argument of perigee: | 84.0132° |
| revolutions per day: | 16.03869813 |
| mean anomaly at epoch: | 112.2864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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