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 41885U 26145.06056654 +.00000000 +00000-0 +32448-3 0 00003
2 41885 34.9340 22.4216 0007883 328.3714 31.6537 15.60045850 01
| Epoch (UTC): | 25 May 2026 01:27:12 |
| Eccentricity: | 0.0007883 |
| inclination: | 34.9340° |
| perigee height: | 382 km |
| apogee height: | 393 km |
| right ascension of ascending node: | 22.4216° |
| argument of perigee: | 328.3714° |
| revolutions per day: | 15.60045850 |
| mean anomaly at epoch: | 31.6537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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