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 49736U 26145.43631670 +.00000000 +00000-0 +30189-4 0 00005
2 49736 53.2129 164.4738 0001107 70.3050 289.8061 15.08836535 08
| Epoch (UTC): | 25 May 2026 10:28:17 |
| Eccentricity: | 0.0001107 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 164.4738° |
| argument of perigee: | 70.3050° |
| revolutions per day: | 15.08836535 |
| mean anomaly at epoch: | 289.8061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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