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 66282U 26145.51549310 +.00000000 +00000-0 +25086-3 0 00007
2 66282 53.1590 194.7628 0001223 84.2673 275.8467 15.30199811 01
| Epoch (UTC): | 25 May 2026 12:22:18 |
| Eccentricity: | 0.0001223 |
| inclination: | 53.1590° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.7628° |
| argument of perigee: | 84.2673° |
| revolutions per day: | 15.30199811 |
| mean anomaly at epoch: | 275.8467° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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