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 49422U 26145.56612602 +.00000000 +00000-0 +29262-3 0 00004
2 49422 53.2153 244.3262 0001120 90.9377 269.1744 15.08827668 08
| Epoch (UTC): | 25 May 2026 13:35:13 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.2153° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 244.3262° |
| argument of perigee: | 90.9377° |
| revolutions per day: | 15.08827668 |
| mean anomaly at epoch: | 269.1744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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