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 59172U 26144.84407705 +.00000000 +00000-0 +86580-3 0 00009
2 59172 43.0005 350.1291 0001583 268.9947 91.0723 15.27592496 03
| Epoch (UTC): | 24 May 2026 20:15:28 |
| Eccentricity: | 0.0001583 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 350.1291° |
| argument of perigee: | 268.9947° |
| revolutions per day: | 15.27592496 |
| mean anomaly at epoch: | 91.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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