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 62713U 26145.13200661 +.00000000 +00000-0 +46785-3 0 00002
2 62713 97.6986 226.7284 0008623 179.1723 180.9517 15.00867455 08
| Epoch (UTC): | 25 May 2026 03:10:05 |
| Eccentricity: | 0.0008623 |
| inclination: | 97.6986° |
| perigee height: | 558 km |
| apogee height: | 570 km |
| right ascension of ascending node: | 226.7284° |
| argument of perigee: | 179.1723° |
| revolutions per day: | 15.00867455 |
| mean anomaly at epoch: | 180.9517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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