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 66670U 26145.11590336 +.00000000 +00000-0 +99749-3 0 00005
2 66670 97.4080 219.4820 0008162 100.5899 259.6259 15.25659254 02
| Epoch (UTC): | 25 May 2026 02:46:54 |
| Eccentricity: | 0.0008162 |
| inclination: | 97.4080° |
| perigee height: | 483 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 219.4820° |
| argument of perigee: | 100.5899° |
| revolutions per day: | 15.25659254 |
| mean anomaly at epoch: | 259.6259° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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