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 66637U 26145.27606876 +.00000000 +00000-0 +78948-3 0 00000
2 66637 53.1588 142.6926 0001127 89.2268 270.8863 15.34404554 05
| Epoch (UTC): | 25 May 2026 06:37:32 |
| Eccentricity: | 0.0001127 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 142.6926° |
| argument of perigee: | 89.2268° |
| revolutions per day: | 15.34404554 |
| mean anomaly at epoch: | 270.8863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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