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 26150.49558382 +.00000000 +00000-0 +18875-3 0 00002
2 28649 97.5315 174.3626 0002595 102.5942 257.5567 14.90997939 01
| Epoch (UTC): | 30 May 2026 11:53:38 |
| Eccentricity: | 0.0002595 |
| inclination: | 97.5315° |
| perigee height: | 593 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 174.3626° |
| argument of perigee: | 102.5942° |
| revolutions per day: | 14.90997939 |
| mean anomaly at epoch: | 257.5567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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