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 49773U 26145.35796574 +.00000000 +00000-0 +30590-3 0 00007
2 49773 53.1960 163.0351 0004203 53.6252 306.5143 15.45102864 05
| Epoch (UTC): | 25 May 2026 08:35:28 |
| Eccentricity: | 0.0004203 |
| inclination: | 53.1960° |
| perigee height: | 428 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 163.0351° |
| argument of perigee: | 53.6252° |
| revolutions per day: | 15.45102864 |
| mean anomaly at epoch: | 306.5143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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