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 66260U 26145.65626075 +.00000000 +00000-0 +11154-2 0 00002
2 66260 53.1601 286.1595 0001743 106.1678 253.9515 15.31741159 05
| Epoch (UTC): | 25 May 2026 15:45:00 |
| Eccentricity: | 0.0001743 |
| inclination: | 53.1601° |
| perigee height: | 469 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 286.1595° |
| argument of perigee: | 106.1678° |
| revolutions per day: | 15.31741159 |
| mean anomaly at epoch: | 253.9515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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