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 41879U 26145.21016752 +.00000000 +00000-0 +00000-0 0 00004
2 41879 0.0093 340.0703 0000534 4.2006 124.0069 1.00277359 00
| Epoch (UTC): | 25 May 2026 05:02:38 |
| Eccentricity: | 0.0000534 |
| inclination: | 0.0093° |
| perigee height: | 35783 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 340.0703° |
| argument of perigee: | 4.2006° |
| revolutions per day: | 1.00277359 |
| mean anomaly at epoch: | 124.0069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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