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 26017.96302484 +.00000000 +00000-0 +26193-4 0 00003
2 27464 82.4828 78.9007 0024766 225.1077 134.7993 12.44619512 08
| Epoch (UTC): | 17 January 2026 23:06:45 |
| Eccentricity: | 0.0024766 |
| inclination: | 82.4828° |
| perigee height: | 1468 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 78.9007° |
| argument of perigee: | 225.1077° |
| revolutions per day: | 12.44619512 |
| mean anomaly at epoch: | 134.7993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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