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 49193U 26145.29638385 +.00000000 +00000-0 -48936-4 0 00006
2 49193 87.9170 340.0046 0001756 92.9653 267.1680 13.18685538 08
| Epoch (UTC): | 25 May 2026 07:06:47 |
| Eccentricity: | 0.0001756 |
| inclination: | 87.9170° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0046° |
| argument of perigee: | 92.9653° |
| revolutions per day: | 13.18685538 |
| mean anomaly at epoch: | 267.1680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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