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 57291U 26145.48767451 +.00000000 +00000-0 +10099-4 0 00000
2 57291 43.0013 149.3797 0001566 267.2484 92.8189 15.27577152 07
| Epoch (UTC): | 25 May 2026 11:42:15 |
| Eccentricity: | 0.0001566 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.3797° |
| argument of perigee: | 267.2484° |
| revolutions per day: | 15.27577152 |
| mean anomaly at epoch: | 92.8189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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