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 62673U 26145.16246462 +.00000000 +00000-0 +25721-3 0 00006
2 62673 97.4419 219.3130 0004672 111.0737 249.1001 15.25680419 06
| Epoch (UTC): | 25 May 2026 03:53:56 |
| Eccentricity: | 0.0004672 |
| inclination: | 97.4419° |
| perigee height: | 486 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 219.3130° |
| argument of perigee: | 111.0737° |
| revolutions per day: | 15.25680419 |
| mean anomaly at epoch: | 249.1001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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