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 40505U 26145.52042508 +.00000000 +00000-0 +00000-0 0 00001
2 40505 0.0418 96.2147 0003125 330.2092 44.0414 1.00274436 02
| Epoch (UTC): | 25 May 2026 12:29:24 |
| Eccentricity: | 0.0003125 |
| inclination: | 0.0418° |
| perigee height: | 35773 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 96.2147° |
| argument of perigee: | 330.2092° |
| revolutions per day: | 1.00274436 |
| mean anomaly at epoch: | 44.0414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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