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 57329U 26145.43665235 +.00000000 +00000-0 +14822-4 0 00002
2 57329 43.0022 178.9951 0001342 268.4881 91.5817 15.27575012 02
| Epoch (UTC): | 25 May 2026 10:28:46 |
| Eccentricity: | 0.0001342 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 178.9951° |
| argument of perigee: | 268.4881° |
| revolutions per day: | 15.27575012 |
| mean anomaly at epoch: | 91.5817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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