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 66139U 26145.43444238 +.00000000 +00000-0 +40464-3 0 00009
2 66139 53.1614 42.9190 0001219 101.0974 259.0164 15.30208225 02
| Epoch (UTC): | 25 May 2026 10:25:35 |
| Eccentricity: | 0.0001219 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 42.9190° |
| argument of perigee: | 101.0974° |
| revolutions per day: | 15.30208225 |
| mean anomaly at epoch: | 259.0164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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