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 66950U 26145.02647859 +.00000000 +00000-0 +11914-2 0 00006
2 66950 53.1594 3.2009 0000961 62.0138 298.0962 15.34406766 03
| Epoch (UTC): | 25 May 2026 00:38:07 |
| Eccentricity: | 0.0000961 |
| inclination: | 53.1594° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 3.2009° |
| argument of perigee: | 62.0138° |
| revolutions per day: | 15.34406766 |
| mean anomaly at epoch: | 298.0962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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