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 49020U 26145.62099941 +.00000000 +00000-0 +68953-4 0 00001
2 49020 44.9956 327.9994 0007389 140.0275 220.1106 14.08534118 00
| Epoch (UTC): | 25 May 2026 14:54:14 |
| Eccentricity: | 0.0007389 |
| inclination: | 44.9956° |
| perigee height: | 859 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 327.9994° |
| argument of perigee: | 140.0275° |
| revolutions per day: | 14.08534118 |
| mean anomaly at epoch: | 220.1106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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