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 66489U 26145.41801220 +.00000000 +00000-0 +61396-3 0 00000
2 66489 42.9982 277.3639 0001254 216.0722 144.0045 15.27594832 02
| Epoch (UTC): | 25 May 2026 10:01:56 |
| Eccentricity: | 0.0001254 |
| inclination: | 42.9982° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.3639° |
| argument of perigee: | 216.0722° |
| revolutions per day: | 15.27594832 |
| mean anomaly at epoch: | 144.0045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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