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 40485U 26145.58335647 +.00000000 +00000-0 +00000-0 0 00003
2 40485 71.8291 349.1028 8340873 166.9300 152.7120 0.28352371 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.8340873 |
| inclination: | 71.8291° |
| perigee height: | 9861 km |
| apogee height: | 173135 km |
| right ascension of ascending node: | 349.1028° |
| argument of perigee: | 166.9300° |
| revolutions per day: | 0.28352371 |
| mean anomaly at epoch: | 152.7120° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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