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 49754U 26145.31950176 +.00000000 +00000-0 +10476-3 0 00003
2 49754 53.2129 155.2219 0001189 81.6052 278.5075 15.08847375 01
| Epoch (UTC): | 25 May 2026 07:40:04 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 155.2219° |
| argument of perigee: | 81.6052° |
| revolutions per day: | 15.08847375 |
| mean anomaly at epoch: | 278.5075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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