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 57469U 26145.03341723 +.00000000 +00000-0 -54412-4 0 00006
2 57469 43.0000 268.2992 0001039 295.5775 64.4969 15.27562580 00
| Epoch (UTC): | 25 May 2026 00:48:07 |
| Eccentricity: | 0.0001039 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 268.2992° |
| argument of perigee: | 295.5775° |
| revolutions per day: | 15.27562580 |
| mean anomaly at epoch: | 64.4969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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