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 54338U 26087.99544422 +.00000000 +00000-0 +63379-3 0 00009
2 54338 98.8391 95.4958 0039408 192.3462 167.6749 14.14371526 08
| Epoch (UTC): | 28 March 2026 23:53:26 |
| Eccentricity: | 0.0039408 |
| inclination: | 98.8391° |
| perigee height: | 816 km |
| apogee height: | 873 km |
| right ascension of ascending node: | 95.4958° |
| argument of perigee: | 192.3462° |
| revolutions per day: | 14.14371526 |
| mean anomaly at epoch: | 167.6749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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