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 40141U 26145.60753947 +.00000000 +00000-0 +00000-0 0 00002
2 40141 0.0508 96.7467 0000834 320.2406 164.8381 1.00272255 01
| Epoch (UTC): | 25 May 2026 14:34:51 |
| Eccentricity: | 0.0000834 |
| inclination: | 0.0508° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 96.7467° |
| argument of perigee: | 320.2406° |
| revolutions per day: | 1.00272255 |
| mean anomaly at epoch: | 164.8381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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