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 39419U 26145.60761845 +.00000000 +00000-0 +13362-3 0 00002
2 39419 97.4555 136.3483 0012990 107.4741 252.7910 15.09980987 08
| Epoch (UTC): | 25 May 2026 14:34:58 |
| Eccentricity: | 0.0012990 |
| inclination: | 97.4555° |
| perigee height: | 527 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 136.3483° |
| argument of perigee: | 107.4741° |
| revolutions per day: | 15.09980987 |
| mean anomaly at epoch: | 252.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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