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 66355U 26145.50723722 +.00000000 +00000-0 +68272-3 0 00002
2 66355 53.1600 235.8651 0001725 100.3280 259.7915 15.30215311 01
| Epoch (UTC): | 25 May 2026 12:10:25 |
| Eccentricity: | 0.0001725 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.8651° |
| argument of perigee: | 100.3280° |
| revolutions per day: | 15.30215311 |
| mean anomaly at epoch: | 259.7915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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