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 66152U 26145.07110271 +.00000000 +00000-0 +58176-3 0 00000
2 66152 53.1582 67.2645 0001025 83.3475 276.7645 15.34398988 09
| Epoch (UTC): | 25 May 2026 01:42:23 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 67.2645° |
| argument of perigee: | 83.3475° |
| revolutions per day: | 15.34398988 |
| mean anomaly at epoch: | 276.7645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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