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 62748U 26145.54455809 +.00000000 +00000-0 +59901-3 0 00005
2 62748 42.9988 83.6153 0000243 329.9195 30.1643 15.27583588 01
| Epoch (UTC): | 25 May 2026 13:04:09 |
| Eccentricity: | 0.0000243 |
| inclination: | 42.9988° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 83.6153° |
| argument of perigee: | 329.9195° |
| revolutions per day: | 15.27583588 |
| mean anomaly at epoch: | 30.1643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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