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 66077U 26145.26337576 +.00000000 +00000-0 +66547-3 0 00007
2 66077 53.1581 249.7054 0001465 86.3122 273.8046 15.30209313 07
| Epoch (UTC): | 25 May 2026 06:19:15 |
| Eccentricity: | 0.0001465 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 249.7054° |
| argument of perigee: | 86.3122° |
| revolutions per day: | 15.30209313 |
| mean anomaly at epoch: | 273.8046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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