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 49748U 26145.45101043 +.00000000 +00000-0 +80271-4 0 00003
2 49748 53.2131 164.1021 0001077 92.6480 267.4635 15.08840587 07
| Epoch (UTC): | 25 May 2026 10:49:27 |
| Eccentricity: | 0.0001077 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.1021° |
| argument of perigee: | 92.6480° |
| revolutions per day: | 15.08840587 |
| mean anomaly at epoch: | 267.4635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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