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 41838U 26145.35207044 +.00000000 +00000-0 +00000-0 0 00000
2 41838 5.6974 72.8752 0001861 9.9411 196.9977 0.99854587 01
| Epoch (UTC): | 25 May 2026 08:26:58 |
| Eccentricity: | 0.0001861 |
| inclination: | 5.6974° |
| perigee height: | 35896 km |
| apogee height: | 35912 km |
| right ascension of ascending node: | 72.8752° |
| argument of perigee: | 9.9411° |
| revolutions per day: | 0.99854587 |
| mean anomaly at epoch: | 196.9977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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