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 49076U 26145.55236928 +.00000000 +00000-0 +19419-3 0 00004
2 49076 87.8948 355.1822 0001976 88.6509 271.4846 13.12442183 08
| Epoch (UTC): | 25 May 2026 13:15:24 |
| Eccentricity: | 0.0001976 |
| inclination: | 87.8948° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1822° |
| argument of perigee: | 88.6509° |
| revolutions per day: | 13.12442183 |
| mean anomaly at epoch: | 271.4846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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