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 62409U 26145.15811147 +.00000000 +00000-0 +22628-2 0 00002
2 62409 43.0011 67.0429 0001790 283.7693 76.2975 15.70906817 05
| Epoch (UTC): | 25 May 2026 03:47:40 |
| Eccentricity: | 0.0001790 |
| inclination: | 43.0011° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 67.0429° |
| argument of perigee: | 283.7693° |
| revolutions per day: | 15.70906817 |
| mean anomaly at epoch: | 76.2975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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