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 26145.48031868 +.00000000 +00000-0 +00000-0 0 00004
2 39256 5.2385 67.3980 0088056 188.4219 35.9939 1.00275815 00
| Epoch (UTC): | 25 May 2026 11:31:39 |
| Eccentricity: | 0.0088056 |
| inclination: | 5.2385° |
| perigee height: | 35414 km |
| apogee height: | 36157 km |
| right ascension of ascending node: | 67.3980° |
| argument of perigee: | 188.4219° |
| revolutions per day: | 1.00275815 |
| mean anomaly at epoch: | 35.9939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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