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 62280U 26145.42849473 +.00000000 +00000-0 +63248-3 0 00006
2 62280 43.0010 132.1218 0001825 263.2943 96.7701 15.27593583 09
| Epoch (UTC): | 25 May 2026 10:17:01 |
| Eccentricity: | 0.0001825 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.1218° |
| argument of perigee: | 263.2943° |
| revolutions per day: | 15.27593583 |
| mean anomaly at epoch: | 96.7701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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