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 66202U 26145.56148674 +.00000000 +00000-0 +12184-2 0 00006
2 66202 53.1589 248.1549 0001162 82.4995 277.6138 15.30227870 08
| Epoch (UTC): | 25 May 2026 13:28:32 |
| Eccentricity: | 0.0001162 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.1549° |
| argument of perigee: | 82.4995° |
| revolutions per day: | 15.30227870 |
| mean anomaly at epoch: | 277.6138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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