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 62009U 26145.04389662 +.00000000 +00000-0 +12332-2 0 00009
2 62009 53.1574 25.1473 0001386 62.5243 297.5915 15.69738365 07
| Epoch (UTC): | 25 May 2026 01:03:12 |
| Eccentricity: | 0.0001386 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 25.1473° |
| argument of perigee: | 62.5243° |
| revolutions per day: | 15.69738365 |
| mean anomaly at epoch: | 297.5915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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