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 66894U 26144.96027786 +.00000000 +00000-0 +10261-2 0 00000
2 66894 53.1592 29.7455 0000583 118.6211 241.4848 15.30193983 01
| Epoch (UTC): | 24 May 2026 23:02:48 |
| Eccentricity: | 0.0000583 |
| inclination: | 53.1592° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.7455° |
| argument of perigee: | 118.6211° |
| revolutions per day: | 15.30193983 |
| mean anomaly at epoch: | 241.4848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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