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 57235U 26144.85019484 +.00000000 +00000-0 +71829-4 0 00002
2 57235 43.0028 320.5708 0001519 278.6491 81.4189 15.27573199 09
| Epoch (UTC): | 24 May 2026 20:24:16 |
| Eccentricity: | 0.0001519 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.5708° |
| argument of perigee: | 278.6491° |
| revolutions per day: | 15.27573199 |
| mean anomaly at epoch: | 81.4189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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