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 66774U 26145.15064536 +.00000000 +00000-0 +24145-3 0 00000
2 66774 97.4208 219.4173 0000435 40.3229 319.8039 15.20802730 02
| Epoch (UTC): | 25 May 2026 03:36:55 |
| Eccentricity: | 0.0000435 |
| inclination: | 97.4208° |
| perigee height: | 503 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 219.4173° |
| argument of perigee: | 40.3229° |
| revolutions per day: | 15.20802730 |
| mean anomaly at epoch: | 319.8039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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