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 43017U 26145.58258409 +.00000000 +00000-0 +44979-3 0 00003
2 43017 97.4740 13.2645 0153037 47.1552 314.2419 15.12246380 08
| Epoch (UTC): | 25 May 2026 13:58:55 |
| Eccentricity: | 0.0153037 |
| inclination: | 97.4740° |
| perigee height: | 424 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 13.2645° |
| argument of perigee: | 47.1552° |
| revolutions per day: | 15.12246380 |
| mean anomaly at epoch: | 314.2419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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