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 66084U 26145.14119030 +.00000000 +00000-0 +97253-3 0 00003
2 66084 53.1608 250.3586 0001823 82.4038 277.7169 15.30194420 05
| Epoch (UTC): | 25 May 2026 03:23:18 |
| Eccentricity: | 0.0001823 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 250.3586° |
| argument of perigee: | 82.4038° |
| revolutions per day: | 15.30194420 |
| mean anomaly at epoch: | 277.7169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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