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 40920U 26145.61329170 +.00000000 +00000-0 +71006-3 0 00002
2 40920 82.4904 93.7233 0011011 42.9315 317.2622 12.42926492 03
| Epoch (UTC): | 25 May 2026 14:43:08 |
| Eccentricity: | 0.0011011 |
| inclination: | 82.4904° |
| perigee height: | 1486 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 93.7233° |
| argument of perigee: | 42.9315° |
| revolutions per day: | 12.42926492 |
| mean anomaly at epoch: | 317.2622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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