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 62684U 26145.18958487 +.00000000 +00000-0 +17708-3 0 00003
2 62684 97.3892 225.2195 0006776 79.4189 280.7813 15.26032826 00
| Epoch (UTC): | 25 May 2026 04:33:00 |
| Eccentricity: | 0.0006776 |
| inclination: | 97.3892° |
| perigee height: | 483 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 225.2195° |
| argument of perigee: | 79.4189° |
| revolutions per day: | 15.26032826 |
| mean anomaly at epoch: | 280.7813° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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