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 49300U 26145.66397979 +.00000000 +00000-0 -12385-3 0 00006
2 49300 87.8943 294.1884 0002442 94.7452 265.3957 13.14501714 00
| Epoch (UTC): | 25 May 2026 15:56:07 |
| Eccentricity: | 0.0002442 |
| inclination: | 87.8943° |
| perigee height: | 1204 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 294.1884° |
| argument of perigee: | 94.7452° |
| revolutions per day: | 13.14501714 |
| mean anomaly at epoch: | 265.3957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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