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 59662U 26145.53353302 +.00000000 +00000-0 +22801-4 0 00000
2 59662 43.0022 327.9781 0001108 272.8985 87.1740 15.27572109 05
| Epoch (UTC): | 25 May 2026 12:48:17 |
| Eccentricity: | 0.0001108 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.9781° |
| argument of perigee: | 272.8985° |
| revolutions per day: | 15.27572109 |
| mean anomaly at epoch: | 87.1740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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