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 41380U 26144.96355668 +.00000000 +00000-0 +00000-0 0 00004
2 41380 0.0127 355.7597 0002282 75.7308 266.2486 1.00271553 01
| Epoch (UTC): | 24 May 2026 23:07:31 |
| Eccentricity: | 0.0002282 |
| inclination: | 0.0127° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 355.7597° |
| argument of perigee: | 75.7308° |
| revolutions per day: | 1.00271553 |
| mean anomaly at epoch: | 266.2486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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