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 49214U 26145.49594471 +.00000000 +00000-0 +52531-3 0 00003
2 49214 87.8953 324.7426 0001802 103.7612 256.3718 13.13468303 05
| Epoch (UTC): | 25 May 2026 11:54:09 |
| Eccentricity: | 0.0001802 |
| inclination: | 87.8953° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7426° |
| argument of perigee: | 103.7612° |
| revolutions per day: | 13.13468303 |
| mean anomaly at epoch: | 256.3718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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