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 57049U 26145.61593546 +.00000000 +00000-0 +32777-4 0 00005
2 57049 43.0025 36.5416 0001207 255.7260 104.3457 15.27577387 09
| Epoch (UTC): | 25 May 2026 14:46:56 |
| Eccentricity: | 0.0001207 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 36.5416° |
| argument of perigee: | 255.7260° |
| revolutions per day: | 15.27577387 |
| mean anomaly at epoch: | 104.3457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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