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 62674U 26145.22810508 +.00000000 +00000-0 +39238-3 0 00000
2 62674 97.4054 227.7489 0005414 50.5194 309.6524 15.29591827 01
| Epoch (UTC): | 25 May 2026 05:28:28 |
| Eccentricity: | 0.0005414 |
| inclination: | 97.4054° |
| perigee height: | 473 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 227.7489° |
| argument of perigee: | 50.5194° |
| revolutions per day: | 15.29591827 |
| mean anomaly at epoch: | 309.6524° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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