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 57290U 26145.51886920 +.00000000 +00000-0 +14271-2 0 00000
2 57290 42.9926 152.9884 0003078 81.7851 278.3348 15.23662168 07
| Epoch (UTC): | 25 May 2026 12:27:10 |
| Eccentricity: | 0.0003078 |
| inclination: | 42.9926° |
| perigee height: | 493 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 152.9884° |
| argument of perigee: | 81.7851° |
| revolutions per day: | 15.23662168 |
| mean anomaly at epoch: | 278.3348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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