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 28368U 26097.88591304 +.00000000 +00000-0 +22805-3 0 00002
2 28368 98.1232 76.5135 0001613 59.1573 300.9799 14.83552497 07
| Epoch (UTC): | 07 April 2026 21:15:42 |
| Eccentricity: | 0.0001613 |
| inclination: | 98.1232° |
| perigee height: | 617 km |
| apogee height: | 619 km |
| right ascension of ascending node: | 76.5135° |
| argument of perigee: | 59.1573° |
| revolutions per day: | 14.83552497 |
| mean anomaly at epoch: | 300.9799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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