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 66140U 26145.12475282 +.00000000 +00000-0 +59114-3 0 00002
2 66140 53.1594 44.5448 0001198 81.7708 278.3429 15.30210969 06
| Epoch (UTC): | 25 May 2026 02:59:38 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.5448° |
| argument of perigee: | 81.7708° |
| revolutions per day: | 15.30210969 |
| mean anomaly at epoch: | 278.3429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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