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 61744U 26145.59874979 +.00000000 +00000-0 +48328-3 0 00009
2 61744 97.3005 20.4931 0007982 14.5304 345.6176 15.50552844 01
| Epoch (UTC): | 25 May 2026 14:22:11 |
| Eccentricity: | 0.0007982 |
| inclination: | 97.3005° |
| perigee height: | 410 km |
| apogee height: | 421 km |
| right ascension of ascending node: | 20.4931° |
| argument of perigee: | 14.5304° |
| revolutions per day: | 15.50552844 |
| mean anomaly at epoch: | 345.6176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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