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 26141.27215147 +.00000000 +00000-0 +10251-3 0 00005
2 39492 82.4146 296.9489 0017122 12.8620 347.3035 14.95986607 03
| Epoch (UTC): | 21 May 2026 06:31:53 |
| Eccentricity: | 0.0017122 |
| inclination: | 82.4146° |
| perigee height: | 567 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 296.9489° |
| argument of perigee: | 12.8620° |
| revolutions per day: | 14.95986607 |
| mean anomaly at epoch: | 347.3035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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