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 26138.55397395 +.00000000 +00000-0 +00000-0 0 00004
2 39256 5.2217 67.4601 0088044 188.4394 55.5216 1.00274064 07
| Epoch (UTC): | 18 May 2026 13:17:43 |
| Eccentricity: | 0.0088044 |
| inclination: | 5.2217° |
| perigee height: | 35415 km |
| apogee height: | 36157 km |
| right ascension of ascending node: | 67.4601° |
| argument of perigee: | 188.4394° |
| revolutions per day: | 1.00274064 |
| mean anomaly at epoch: | 55.5216° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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