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 57301U 26145.50822829 +.00000000 +00000-0 +43090-4 0 00003
2 57301 43.0017 149.5253 0001232 279.9160 80.1553 15.27579811 02
| Epoch (UTC): | 25 May 2026 12:11:50 |
| Eccentricity: | 0.0001232 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 149.5253° |
| argument of perigee: | 279.9160° |
| revolutions per day: | 15.27579811 |
| mean anomaly at epoch: | 80.1553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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