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 66788U 26145.46069741 +.00000000 +00000-0 +38058-3 0 00000
2 66788 97.4248 219.4879 0005675 186.9589 173.1569 15.21164956 02
| Epoch (UTC): | 25 May 2026 11:03:24 |
| Eccentricity: | 0.0005675 |
| inclination: | 97.4248° |
| perigee height: | 498 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 219.4879° |
| argument of perigee: | 186.9589° |
| revolutions per day: | 15.21164956 |
| mean anomaly at epoch: | 173.1569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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