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 49090U 26145.52202433 +.00000000 +00000-0 -85137-3 0 00002
2 49090 87.8957 355.1622 0002012 78.2606 281.8749 13.12442144 01
| Epoch (UTC): | 25 May 2026 12:31:42 |
| Eccentricity: | 0.0002012 |
| inclination: | 87.8957° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.1622° |
| argument of perigee: | 78.2606° |
| revolutions per day: | 13.12442144 |
| mean anomaly at epoch: | 281.8749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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