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 62745U 26145.52703192 +.00000000 +00000-0 +64143-4 0 00006
2 62745 43.0022 80.0203 0000064 74.6655 285.4203 15.27601648 07
| Epoch (UTC): | 25 May 2026 12:38:55 |
| Eccentricity: | 0.0000064 |
| inclination: | 43.0022° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 80.0203° |
| argument of perigee: | 74.6655° |
| revolutions per day: | 15.27601648 |
| mean anomaly at epoch: | 285.4203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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