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 57947U 26145.66228684 +.00000000 +00000-0 +83784-4 0 00009
2 57947 53.1616 26.2909 0001229 94.9470 265.1673 15.34397604 03
| Epoch (UTC): | 25 May 2026 15:53:41 |
| Eccentricity: | 0.0001229 |
| inclination: | 53.1616° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 26.2909° |
| argument of perigee: | 94.9470° |
| revolutions per day: | 15.34397604 |
| mean anomaly at epoch: | 265.1673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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