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 26145.60013031 +.00000000 +00000-0 +39719-3 0 00001
2 28419 82.4857 340.0186 0015442 321.0217 38.9750 12.45679186 05
| Epoch (UTC): | 25 May 2026 14:24:11 |
| Eccentricity: | 0.0015442 |
| inclination: | 82.4857° |
| perigee height: | 1470 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 340.0186° |
| argument of perigee: | 321.0217° |
| revolutions per day: | 12.45679186 |
| mean anomaly at epoch: | 38.9750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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