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 40960U 26145.65069292 +.00000000 +00000-0 +81510-4 0 00008
2 40960 97.6588 142.7358 0016729 348.4844 11.5983 14.77461181 01
| Epoch (UTC): | 25 May 2026 15:36:59 |
| Eccentricity: | 0.0016729 |
| inclination: | 97.6588° |
| perigee height: | 626 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 142.7358° |
| argument of perigee: | 348.4844° |
| revolutions per day: | 14.77461181 |
| mean anomaly at epoch: | 11.5983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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