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 28419U 26109.45762961 +.00000000 +00000-0 +61470-3 0 00006
2 28419 82.4904 2.6599 0016892 39.2488 320.9815 12.45677886 06
| Epoch (UTC): | 19 April 2026 10:58:59 |
| Eccentricity: | 0.0016892 |
| inclination: | 82.4904° |
| perigee height: | 1469 km |
| apogee height: | 1496 km |
| right ascension of ascending node: | 2.6599° |
| argument of perigee: | 39.2488° |
| revolutions per day: | 12.45677886 |
| mean anomaly at epoch: | 320.9815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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