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 66938U 26144.98659095 +.00000000 +00000-0 +47690-3 0 00002
2 66938 53.1601 3.6680 0000918 85.3475 274.7633 15.34409689 04
| Epoch (UTC): | 24 May 2026 23:40:41 |
| Eccentricity: | 0.0000918 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 3.6680° |
| argument of perigee: | 85.3475° |
| revolutions per day: | 15.34409689 |
| mean anomaly at epoch: | 274.7633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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