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 66138U 26145.41345115 +.00000000 +00000-0 +43172-3 0 00009
2 66138 53.1585 43.5010 0000947 90.2761 269.8348 15.30209668 01
| Epoch (UTC): | 25 May 2026 09:55:22 |
| Eccentricity: | 0.0000947 |
| inclination: | 53.1585° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.5010° |
| argument of perigee: | 90.2761° |
| revolutions per day: | 15.30209668 |
| mean anomaly at epoch: | 269.8348° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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