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 66162U 26145.19796516 +.00000000 +00000-0 +94160-3 0 00009
2 66162 53.1587 67.3251 0001637 89.6046 270.5142 15.30233029 05
| Epoch (UTC): | 25 May 2026 04:45:04 |
| Eccentricity: | 0.0001637 |
| inclination: | 53.1587° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 67.3251° |
| argument of perigee: | 89.6046° |
| revolutions per day: | 15.30233029 |
| mean anomaly at epoch: | 270.5142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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