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 49390U 26145.47228368 +.00000000 +00000-0 +31328-3 0 00006
2 49390 34.9906 59.5398 0005597 185.0138 175.0522 15.26218735 01
| Epoch (UTC): | 25 May 2026 11:20:05 |
| Eccentricity: | 0.0005597 |
| inclination: | 34.9906° |
| perigee height: | 483 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 59.5398° |
| argument of perigee: | 185.0138° |
| revolutions per day: | 15.26218735 |
| mean anomaly at epoch: | 175.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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