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 66197U 26145.56886338 +.00000000 +00000-0 +15011-3 0 00008
2 66197 53.1587 248.2085 0001283 93.8402 266.2745 15.30197981 05
| Epoch (UTC): | 25 May 2026 13:39:09 |
| Eccentricity: | 0.0001283 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.2085° |
| argument of perigee: | 93.8402° |
| revolutions per day: | 15.30197981 |
| mean anomaly at epoch: | 266.2745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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