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 10489U 26138.89738405 +.00000000 +00000-0 +00000-0 0 00009
2 10489 5.1489 281.5089 0010534 98.5229 201.0803 1.00320336 04
| Epoch (UTC): | 18 May 2026 21:32:13 |
| Eccentricity: | 0.0010534 |
| inclination: | 5.1489° |
| perigee height: | 35729 km |
| apogee height: | 35817 km |
| right ascension of ascending node: | 281.5089° |
| argument of perigee: | 98.5229° |
| revolutions per day: | 1.00320336 |
| mean anomaly at epoch: | 201.0803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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