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 66507U 26145.43729281 +.00000000 +00000-0 +10045-2 0 00003
2 66507 43.0009 277.5131 0001143 248.4354 111.6376 15.27594207 04
| Epoch (UTC): | 25 May 2026 10:29:42 |
| Eccentricity: | 0.0001143 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.5131° |
| argument of perigee: | 248.4354° |
| revolutions per day: | 15.27594207 |
| mean anomaly at epoch: | 111.6376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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