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 59465U 26145.53315277 +.00000000 +00000-0 +65939-5 0 00000
2 59465 43.0033 320.6708 0000758 274.0322 86.0443 15.27573303 01
| Epoch (UTC): | 25 May 2026 12:47:44 |
| Eccentricity: | 0.0000758 |
| inclination: | 43.0033° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.6708° |
| argument of perigee: | 274.0322° |
| revolutions per day: | 15.27573303 |
| mean anomaly at epoch: | 86.0443° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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