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 66141U 26044.57166178 +.00000000 +00000-0 +75205-3 0 00000
2 66141 53.1601 151.9535 0001178 88.0781 272.0355 15.30200814 02
| Epoch (UTC): | 13 February 2026 13:43:11 |
| Eccentricity: | 0.0001178 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 151.9535° |
| argument of perigee: | 88.0781° |
| revolutions per day: | 15.30200814 |
| mean anomaly at epoch: | 272.0355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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