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 48049U 26145.44262329 +.00000000 +00000-0 -70762-3 0 00004
2 48049 87.8941 324.7580 0001631 92.1771 267.9545 13.13468861 00
| Epoch (UTC): | 25 May 2026 10:37:22 |
| Eccentricity: | 0.0001631 |
| inclination: | 87.8941° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7580° |
| argument of perigee: | 92.1771° |
| revolutions per day: | 13.13468861 |
| mean anomaly at epoch: | 267.9545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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