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 28649U 26070.56102277 +.00000000 +00000-0 +22152-3 0 00002
2 28649 97.5415 98.0249 0002320 67.4781 292.6683 14.90774349 08
| Epoch (UTC): | 11 March 2026 13:27:52 |
| Eccentricity: | 0.0002320 |
| inclination: | 97.5415° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 98.0249° |
| argument of perigee: | 67.4781° |
| revolutions per day: | 14.90774349 |
| mean anomaly at epoch: | 292.6683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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