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 66154U 26145.47716873 +.00000000 +00000-0 +54431-3 0 00006
2 66154 53.1587 66.2343 0001120 98.2671 261.8457 15.30208954 04
| Epoch (UTC): | 25 May 2026 11:27:07 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 66.2343° |
| argument of perigee: | 98.2671° |
| revolutions per day: | 15.30208954 |
| mean anomaly at epoch: | 261.8457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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