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 49735U 26145.47955551 +.00000000 +00000-0 +11323-3 0 00003
2 49735 53.2127 174.2830 0001658 59.8541 300.2615 15.08854171 04
| Epoch (UTC): | 25 May 2026 11:30:33 |
| Eccentricity: | 0.0001658 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 174.2830° |
| argument of perigee: | 59.8541° |
| revolutions per day: | 15.08854171 |
| mean anomaly at epoch: | 300.2615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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