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 66135U 26145.14058550 +.00000000 +00000-0 +76150-3 0 00002
2 66135 53.1582 44.6453 0001125 85.9818 274.1311 15.30207115 05
| Epoch (UTC): | 25 May 2026 03:22:26 |
| Eccentricity: | 0.0001125 |
| inclination: | 53.1582° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.6453° |
| argument of perigee: | 85.9818° |
| revolutions per day: | 15.30207115 |
| mean anomaly at epoch: | 274.1311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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