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 49059U 26145.61029997 +.00000000 +00000-0 +13786-4 0 00000
2 49059 89.0056 221.0056 0003715 95.4027 264.7573 13.94389063 06
| Epoch (UTC): | 25 May 2026 14:38:49 |
| Eccentricity: | 0.0003715 |
| inclination: | 89.0056° |
| perigee height: | 911 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 221.0056° |
| argument of perigee: | 95.4027° |
| revolutions per day: | 13.94389063 |
| mean anomaly at epoch: | 264.7573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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