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 49413U 26145.41612822 +.00000000 +00000-0 +19081-4 0 00001
2 49413 53.2135 234.6929 0001246 80.9837 279.1296 15.08835215 09
| Epoch (UTC): | 25 May 2026 09:59:13 |
| Eccentricity: | 0.0001246 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 234.6929° |
| argument of perigee: | 80.9837° |
| revolutions per day: | 15.08835215 |
| mean anomaly at epoch: | 279.1296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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