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 49218U 26145.50539169 +.00000000 +00000-0 +18703-3 0 00005
2 49218 87.8930 324.7544 0001608 96.2352 263.8960 13.13468411 08
| Epoch (UTC): | 25 May 2026 12:07:45 |
| Eccentricity: | 0.0001608 |
| inclination: | 87.8930° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7544° |
| argument of perigee: | 96.2352° |
| revolutions per day: | 13.13468411 |
| mean anomaly at epoch: | 263.8960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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