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 49261U 26145.12198705 +.00000000 +00000-0 +45753-3 0 00003
2 49261 97.3780 208.4063 0013242 156.5898 203.5950 15.33968854 01
| Epoch (UTC): | 25 May 2026 02:55:39 |
| Eccentricity: | 0.0013242 |
| inclination: | 97.3780° |
| perigee height: | 455 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 208.4063° |
| argument of perigee: | 156.5898° |
| revolutions per day: | 15.33968854 |
| mean anomaly at epoch: | 203.5950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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