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 26068.54739103 +.00000000 +00000-0 +24542-3 0 00006
2 28649 97.5412 96.1008 0002346 69.8165 290.3306 14.90764799 02
| Epoch (UTC): | 09 March 2026 13:08:14 |
| Eccentricity: | 0.0002346 |
| inclination: | 97.5412° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 96.1008° |
| argument of perigee: | 69.8165° |
| revolutions per day: | 14.90764799 |
| mean anomaly at epoch: | 290.3306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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