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 62411U 26145.13156336 +.00000000 +00000-0 +14828-2 0 00008
2 62411 43.0016 66.8262 0002205 257.2023 102.8598 15.70887422 07
| Epoch (UTC): | 25 May 2026 03:09:27 |
| Eccentricity: | 0.0002205 |
| inclination: | 43.0016° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 66.8262° |
| argument of perigee: | 257.2023° |
| revolutions per day: | 15.70887422 |
| mean anomaly at epoch: | 102.8598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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