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 40887U 26145.17083580 +.00000000 +00000-0 +00000-0 0 00000
2 40887 4.2888 42.1114 0059982 3.6340 333.5154 1.00272577 06
| Epoch (UTC): | 25 May 2026 04:06:00 |
| Eccentricity: | 0.0059982 |
| inclination: | 4.2888° |
| perigee height: | 35533 km |
| apogee height: | 36039 km |
| right ascension of ascending node: | 42.1114° |
| argument of perigee: | 3.6340° |
| revolutions per day: | 1.00272577 |
| mean anomaly at epoch: | 333.5154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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