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 26067.94329848 +.00000000 +00000-0 +25355-3 0 00003
2 28649 97.5412 95.5237 0002373 70.4785 289.6690 14.90762382 08
| Epoch (UTC): | 08 March 2026 22:38:20 |
| Eccentricity: | 0.0002373 |
| inclination: | 97.5412° |
| perigee height: | 594 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 95.5237° |
| argument of perigee: | 70.4785° |
| revolutions per day: | 14.90762382 |
| mean anomaly at epoch: | 289.6690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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