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 57629U 26145.60465071 +.00000000 +00000-0 +19196-3 0 00008
2 57629 45.0050 46.0812 0006412 151.5358 208.5852 14.62878778 05
| Epoch (UTC): | 25 May 2026 14:30:41 |
| Eccentricity: | 0.0006412 |
| inclination: | 45.0050° |
| perigee height: | 679 km |
| apogee height: | 688 km |
| right ascension of ascending node: | 46.0812° |
| argument of perigee: | 151.5358° |
| revolutions per day: | 14.62878778 |
| mean anomaly at epoch: | 208.5852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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