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 62604U 26145.16162404 +.00000000 +00000-0 +36822-3 0 00007
2 62604 43.0018 205.7150 0001907 273.3647 86.6986 15.27586561 04
| Epoch (UTC): | 25 May 2026 03:52:44 |
| Eccentricity: | 0.0001907 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 205.7150° |
| argument of perigee: | 273.3647° |
| revolutions per day: | 15.27586561 |
| mean anomaly at epoch: | 86.6986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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