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 66215U 26145.50762778 +.00000000 +00000-0 +57318-3 0 00000
2 66215 53.1588 232.8888 0001752 83.6128 276.5072 15.30215651 02
| Epoch (UTC): | 25 May 2026 12:10:59 |
| Eccentricity: | 0.0001752 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 232.8888° |
| argument of perigee: | 83.6128° |
| revolutions per day: | 15.30215651 |
| mean anomaly at epoch: | 276.5072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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