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 49446U 26145.51544381 +.00000000 +00000-0 -13567-3 0 00005
2 49446 53.2120 224.2359 0000983 97.3691 262.7412 15.08853815 02
| Epoch (UTC): | 25 May 2026 12:22:14 |
| Eccentricity: | 0.0000983 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 224.2359° |
| argument of perigee: | 97.3691° |
| revolutions per day: | 15.08853815 |
| mean anomaly at epoch: | 262.7412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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