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 62368U 26145.47640174 +.00000000 +00000-0 +11925-3 0 00000
2 62368 44.9853 62.5590 0008965 273.1335 86.8472 13.99209964 06
| Epoch (UTC): | 25 May 2026 11:26:01 |
| Eccentricity: | 0.0008965 |
| inclination: | 44.9853° |
| perigee height: | 890 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 62.5590° |
| argument of perigee: | 273.1335° |
| revolutions per day: | 13.99209964 |
| mean anomaly at epoch: | 86.8472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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