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 04256U 26133.13565302 +.00000000 +00000-0 +66506-4 0 00007
2 04256 70.0110 40.3138 0017181 114.5275 245.7626 13.99187303 06
| Epoch (UTC): | 13 May 2026 03:15:20 |
| Eccentricity: | 0.0017181 |
| inclination: | 70.0110° |
| perigee height: | 884 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 40.3138° |
| argument of perigee: | 114.5275° |
| revolutions per day: | 13.99187303 |
| mean anomaly at epoch: | 245.7626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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