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 39256U 26145.91558264 +.00000000 +00000-0 +00000-0 0 00006
2 39256 5.2395 67.3943 0088051 188.4267 193.1230 1.00275919 04
| Epoch (UTC): | 25 May 2026 21:58:26 |
| Eccentricity: | 0.0088051 |
| inclination: | 5.2395° |
| perigee height: | 35414 km |
| apogee height: | 36157 km |
| right ascension of ascending node: | 67.3943° |
| argument of perigee: | 188.4267° |
| revolutions per day: | 1.00275919 |
| mean anomaly at epoch: | 193.1230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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