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 59460U 26145.52464197 +.00000000 +00000-0 +14810-3 0 00000
2 59460 43.0025 317.1364 0000915 269.1747 90.9000 15.27554098 00
| Epoch (UTC): | 25 May 2026 12:35:29 |
| Eccentricity: | 0.0000915 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 317.1364° |
| argument of perigee: | 269.1747° |
| revolutions per day: | 15.27554098 |
| mean anomaly at epoch: | 90.9000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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