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 40965U 26145.50600750 +.00000000 +00000-0 +27022-3 0 00004
2 40965 64.7680 333.1439 0130063 72.1997 289.3256 14.91310091 05
| Epoch (UTC): | 25 May 2026 12:08:39 |
| Eccentricity: | 0.0130063 |
| inclination: | 64.7680° |
| perigee height: | 503 km |
| apogee height: | 685 km |
| right ascension of ascending node: | 333.1439° |
| argument of perigee: | 72.1997° |
| revolutions per day: | 14.91310091 |
| mean anomaly at epoch: | 289.3256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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