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 48669U 26145.30004389 +.00000000 +00000-0 +99178-5 0 00000
2 48669 53.1584 107.7605 0001067 85.9114 274.2009 15.31703405 02
| Epoch (UTC): | 25 May 2026 07:12:03 |
| Eccentricity: | 0.0001067 |
| inclination: | 53.1584° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 107.7605° |
| argument of perigee: | 85.9114° |
| revolutions per day: | 15.31703405 |
| mean anomaly at epoch: | 274.2009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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