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 39491U 26145.60763109 +.00000000 +00000-0 +20325-3 0 00004
2 39491 82.4106 272.7569 0014423 282.0678 77.8932 15.04699425 05
| Epoch (UTC): | 25 May 2026 14:34:59 |
| Eccentricity: | 0.0014423 |
| inclination: | 82.4106° |
| perigee height: | 542 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 272.7569° |
| argument of perigee: | 282.0678° |
| revolutions per day: | 15.04699425 |
| mean anomaly at epoch: | 77.8932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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