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 57224U 26145.48735362 +.00000000 +00000-0 +31281-4 0 00008
2 57224 43.0020 316.7559 0001543 259.9142 100.1536 15.27577452 03
| Epoch (UTC): | 25 May 2026 11:41:47 |
| Eccentricity: | 0.0001543 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.7559° |
| argument of perigee: | 259.9142° |
| revolutions per day: | 15.27577452 |
| mean anomaly at epoch: | 100.1536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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