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 62558U 26145.05656516 +.00000000 +00000-0 +10354-2 0 00006
2 62558 42.9986 39.5147 0001915 274.5740 85.4909 15.70834955 02
| Epoch (UTC): | 25 May 2026 01:21:27 |
| Eccentricity: | 0.0001915 |
| inclination: | 42.9986° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 39.5147° |
| argument of perigee: | 274.5740° |
| revolutions per day: | 15.70834955 |
| mean anomaly at epoch: | 85.4909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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