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 64123U 26145.61338841 +.00000000 +00000-0 +14172-2 0 00008
2 64123 43.0031 230.4992 0002253 270.5135 89.5475 15.70869725 01
| Epoch (UTC): | 25 May 2026 14:43:16 |
| Eccentricity: | 0.0002253 |
| inclination: | 43.0031° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 230.4992° |
| argument of perigee: | 270.5135° |
| revolutions per day: | 15.70869725 |
| mean anomaly at epoch: | 89.5475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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