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 49089U 26145.30940404 +.00000000 +00000-0 -92444-3 0 00002
2 49089 87.8959 355.2058 0002113 80.8697 279.2670 13.12443485 09
| Epoch (UTC): | 25 May 2026 07:25:32 |
| Eccentricity: | 0.0002113 |
| inclination: | 87.8959° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2058° |
| argument of perigee: | 80.8697° |
| revolutions per day: | 13.12443485 |
| mean anomaly at epoch: | 279.2670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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