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 66367U 26145.51978756 +.00000000 +00000-0 +60176-3 0 00000
2 66367 53.1594 235.2294 0001233 89.3586 270.7556 15.30199270 01
| Epoch (UTC): | 25 May 2026 12:28:29 |
| Eccentricity: | 0.0001233 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.2294° |
| argument of perigee: | 89.3586° |
| revolutions per day: | 15.30199270 |
| mean anomaly at epoch: | 270.7556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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