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 39250U 26145.62760190 +.00000000 +00000-0 +41114-3 0 00005
2 39250 82.4873 358.3441 0018372 297.4834 62.4377 12.43030151 08
| Epoch (UTC): | 25 May 2026 15:03:44 |
| Eccentricity: | 0.0018372 |
| inclination: | 82.4873° |
| perigee height: | 1479 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 358.3441° |
| argument of perigee: | 297.4834° |
| revolutions per day: | 12.43030151 |
| mean anomaly at epoch: | 62.4377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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