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 48269U 26145.45501863 +.00000000 +00000-0 +96640-3 0 00000
2 48269 97.5766 223.1675 0001184 26.6301 333.5002 15.32738197 01
| Epoch (UTC): | 25 May 2026 10:55:13 |
| Eccentricity: | 0.0001184 |
| inclination: | 97.5766° |
| perigee height: | 467 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 223.1675° |
| argument of perigee: | 26.6301° |
| revolutions per day: | 15.32738197 |
| mean anomaly at epoch: | 333.5002° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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