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 26075.15142384 +.00000000 +00000-0 +40764-3 0 00000
2 43017 97.4857 304.3123 0153612 289.7330 68.7387 15.11027162 08
| Epoch (UTC): | 16 March 2026 03:38:03 |
| Eccentricity: | 0.0153612 |
| inclination: | 97.4857° |
| perigee height: | 427 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 304.3123° |
| argument of perigee: | 289.7330° |
| revolutions per day: | 15.11027162 |
| mean anomaly at epoch: | 68.7387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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