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 57364U 26145.52659809 +.00000000 +00000-0 +33783-4 0 00008
2 57364 43.0030 167.4785 0001974 300.7967 59.2690 15.26742629 03
| Epoch (UTC): | 25 May 2026 12:38:18 |
| Eccentricity: | 0.0001974 |
| inclination: | 43.0030° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 167.4785° |
| argument of perigee: | 300.7967° |
| revolutions per day: | 15.26742629 |
| mean anomaly at epoch: | 59.2690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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