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 39492U 26145.15159361 +.00000000 +00000-0 +94986-4 0 00009
2 39492 82.4144 293.1905 0016807 0.5437 359.5800 14.95992902 02
| Epoch (UTC): | 25 May 2026 03:38:17 |
| Eccentricity: | 0.0016807 |
| inclination: | 82.4144° |
| perigee height: | 568 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 293.1905° |
| argument of perigee: | 0.5437° |
| revolutions per day: | 14.95992902 |
| mean anomaly at epoch: | 359.5800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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