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 27464U 26104.21622729 +.00000000 +00000-0 +11104-3 0 00000
2 27464 82.4881 24.9510 0026496 39.7224 320.5790 12.44621345 09
| Epoch (UTC): | 14 April 2026 05:11:22 |
| Eccentricity: | 0.0026496 |
| inclination: | 82.4881° |
| perigee height: | 1466 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 24.9510° |
| argument of perigee: | 39.7224° |
| revolutions per day: | 12.44621345 |
| mean anomaly at epoch: | 320.5790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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